Software Tenders

Details: Nsn 7r-1660-016884617-qe, Tdp Ver 001, Qty 26 Ea, Delivery Fob Origin. This Part Requires Engineering Source Approval By The Design Control Activity In Order To Maintain The Quality Of The Part. Existing Unique Design Capability, Engineering Skills, And Manufacturing/repair Knowledge By The Qualified Source(s) Require Acquisition/repair Of The Part From The Approved Source(s). The Approved Source(s) Retain Data Rights,manufacturing/repair Knowledge, Or Technical Data That Are Not Economically Available To The Government, And The Data Or Knowledge Is Essential To Maintaining The Quality Of The Part. An Alternate Source Must Qualify In Accordance With The Design Control Activity's Procedures, As Approved By The Cognizant Government Engineering Activity. The Qualification Procedures Must Be Approved By The Government Engineering Activity Having Jurisdiction Over The Part In The Intended Application. The Subject Item Requires Government Source Approval Prior To Contract Award, As The Item Is Flight Critical And/or The Technical Data Available Has Not Been Determined Adequate To Support Acquisition Via Full And Open Competition. Only The Source(s) Previously Approved By The Government For This Item Have Been Solicited. The Time Required For Approval Of A New Source Is Normally Such That An Award Cannot Be Delayed Pending Approval Of A New Source. If You Are Not An Approved Source You Must Submit, Together With Your Proposal, The Information Detailed In One Of The Navsup Weapon Systems Support (navsup Wss) Source Approval Information Brochures Listed Below. Spares: Https://www.navsup.navy.mil/navsup-enterprise/navsup-weapon-systems-sup Port/business-opps/ Repair: Https://www.navsup.navy.mil/navsup-enterprise/navsup -weapon-systems-support/business-opps/ Technical Data Required To Be Submitted Based On Your Company's Experience In Production Of The Same Or Similar Item, Or If This Is An Item You Have Never Made. If Your Request For Source Approval Is Currently Being Evaluated At Navsup Wss Submit With Your Offer A Copy Of The Cover Letter Which Forwarded Your Request For Source Approval. Offers Received Which Fail To Provide All Data Required By The Source Approval Brochure Or Document Previous Submission Of All Data Required By The Source Approval Brochure Will Not Be Considered For Award Under This Solicitation. Please Note, If Evaluation Of A Source Approval Request Submitted Hereunder Cannot Be Processed In Time And/or Approval Requirements Preclude The Ability To Obtain Subject Items In Time To Meet Government Requirements, Award Of The Subject Requirement May Continue Based On Fleet Support Needs. The Navsup Wss Commercial Item Identification Brochure Is Now Available At: "https://www.navsup.navy.mil/navsup-enterprise/navsup-weapon-systems-support/bus Iness-opps/" Interested Parties May Obtain Copies Of Military And Federal Specificationsand Standards, Qualified Products Lists (qpls), Qualified Product Databases(qpds), Military Handbooks, And Other Standardized Documents From The Dodsingle Stock Point (dodssp) At Document Automation And Production Service(daps) In Philadelphia, Pa. Note: Patterns, Drawings, Deviation Lists, Purchase Descriptions, Etc. Are Not Stocked At Dodssp. Most Documents Are Available In Adobe Pdf Format From Assist-online At: Http://quicksearch.dla.mil/. Users May Use Assist-quick Search To Search For And Download Available Documents Directly Using Standard Browser Software. Documents That Are Not Available For Downloading From Assist-quick Search Can Be Ordered From The Dodssp Website Using The Assist Shopping Wizard After Obtaining A Dodssp Customer Account By Following The Registration Procedures. Users Who Do Not Have Access To The Internet May Contact The Dodssp Assisthelp Desk At 215-697-2667 Or 215-697-2179 (dsn: 442-2667), Or Mail Their Request To Dladocument Services, Bldg. 4/d, 700 Robbins Avenue, Philadelphia Pa 19111-5094. The Proposed Contract Action Is For Supplies Or Services For Which The Government Intends To Solicit And Negotiate With Only One Source Under The Authority Of Far 6.302-1. All Responsible Sources May Identify Their Interest And Capability To Respond To The Requirement Or Submit Proposals, Quotationsor Capability Statements. This Notice Of Intent Is Not A Request Forcompetitive Proposals. However, All Proposals Received Within 45 Days (30days If Award Is Issued Under An Existing Basic Ordering Agreement (boa) Afterdate Of Publication Of This Synopsis Will Be Considered By The Government. A Determination By The Government Not To Compete With This Proposed Contract Based Upon Responses To This Notice Is Solely Within The Discretion Of The Government. Information Received Will Normally Be Considered Solely For The Purpose Of Determining Whether To Conduct A Competitive Procurement.

Details: Combined Synopsis/solicitation – Boundary Line Maintenance For B. Everett Jordan Lake, Moncure, Nc solicitation No. W912pm25q0006. This Solicitation Is Issued As An Rfq. this Is A Combined Synopsis/solicitation For Commercial Items Prepared In Accordance With The Format In Far Subpart 12.6 – Streamlined Procedures For Evaluation And Solicitation For Commercial Products And Commercial Services, As Supplemented With Additional Information Included In This Notice. This Announcement Constitutes The Only Solicitation; Quotations Are Being Requested And A Separate Written Solicitation Will Not Be Issued. This Solicitation Is Being Issued Under The Authority Of Far Part 13 Simplified Acquisition Procedures. This Combined Synopsis/solicitation Is Being Issued As A Small Business Set-aside. this Solicitation Is A Request For Quote (rfq). This Solicitation Document Incorporates Provisions And Clauses In Effect Through Federal Acquisition Circular (fac) 2025-01 Effective November 12, 2024. The Associated North American Industry Classification System (naics) Code For This Procurement Is 561730 With A Size Standard Of $9,500,000.00. the U.s. Army Corps Of Engineers, Wilmington District Is Requesting Services Brush And Tree Limb Cutting, Painting, And Signing Approximately 41 Miles Of Existing United States Government’s Property Boundary To Maintain A Highly Visible Boundary Line At B. Everett Jordan Lake. The Contractor Shall Not Be Establishing New Boundary Lines Or Conducting Any Land Survey Activities. the Resulting Award Issued From This Request Will Result In One Award. Service Contract Act Wage Determination 2015-4393 Rev 27, Dated 07-22-2024 For Wake County, Nc And 2015-4373, Rev 27, Dated 07-22-2024 For Chatham County, Nc Will Apply. The Offeror Is Responsible For Referring To The Wage Determination And Applying It As Applicable. the Following Documents Have Been Provided: a21 - Combined Synopsis-solicitation – Bej Boundary Line Maintenance – W912pm25q0006 - Final questions Are Due Not Later Than 4:00 Pm, Edt, 08 January 2025. quotes Are Due Not Later Than 2:00 Pm, Edt, 17 January 2025. submit Questions & Quotes Electronically Via Email To Both Shaun.m.mckenna@usace.army.mil And Jenifer.m.garland@usace.army.mil. It Is Your Responsibility To Follow Up And Ensure Quotes Have Been Received By The Contract Specialist Prior To The Due Date And Time For Quotes. evaluation Of Award: The Government Will Award A Contract Resulting From This Solicitation To The Responsible Offeror Whose Offer Conforming To The Solicitation Will Be Most Advantageous To The Government, Price And Other Factors Considered. Issuance Of Award Will Be Made To The Lowest Price Offeror That Is Technically Acceptable. price Quote And Technical Proposal: Each Offeror Must Submit Both A Price Quote And A Technical Proposal Via Email. The Technical Proposal Shall Include The Documentation In Certification And Documented Past Experience. See Provision 52.212-2 Within The Solicitation. No Hard Copies Will Be Accepted Or Evaluated. Both The Price Quote And Technical Proposal Must Be Received By The Closing Date And Time Set Forth Within The Solicitation. In An Effort To Reduce Paper And Cost, All Quotes Shall Be Submitted Electronically. All Submissions Shall Be In Adobe Pdf Format And Shall Be On 8 ½ X 11 Size Pages In No Less Than 10 Pitch Or 10 Fonts. The Pricing Quote Can Be In Microsoft Excel Spreadsheet Format Provided Within The Solicitation. Offerors May Use Compression Utility Software Such As Winzip Or Pkzip To Reduce Fie Size And Facilitate Electronic Transmission. title File(s) In The Following Format: w912pm25q0006_company Name_pricing w912pm25q0006_company Name_technical in Accordance With Far 52.212-1(k), Each Prospective Awardee Shall Be Registered And Be Active In The Sam Database Prior To Award. If The Offeror Does Not Become Registered In The Sam Database In The Time Prescribed By The Contracting Officer (nlt Due Date/time Of Solicitation), The Contracting Officer Will Proceed To Award To The Next Otherwise Successful Registered Offeror. Offerors May Obtain Information On Registration And Annual Confirmation Requirements Via The Internet At Https://www.sam.gov Or By Calling 866-606-8220, Monday – Friday From 8am – 8pm Est. the Government Reserves The Right To Cancel This Solicitation. this Announcement And Written Request For Quote Constitutes The Only “request For Quote” That Will Be Made For This Requirement.

Details: Nsn 7r-5998-014744622-v2, Tdp Ver 013, Qty 37 Ea, Delivery Fob Origin. This Part Requires Engineering Source Approval By The Design Control Activity In Order To Maintain The Quality Of The Part. Existing Unique Design Capability, Engineering Skills, And Manufacturing/repair Knowledge By The Qualified Source(s) Require Acquisition/repair Of The Part From The Approved Source(s). The Approved Source(s) Retain Data Rights,manufacturing/repair Knowledge, Or Technical Data That Are Not Economically Available To The Government, And The Data Or Knowledge Is Essential To Maintaining The Quality Of The Part. An Alternate Source Must Qualify In Accordance With The Design Control Activity's Procedures, As Approved By The Cognizant Government Engineering Activity. The Qualification Procedures Must Be Approved By The Government Engineering Activity Having Jurisdiction Over The Part In The Intended Application. The Subject Item Requires Government Source Approval Prior To Contract Award, As The Item Is Flight Critical And/or The Technical Data Available Has Not Been Determined Adequate To Support Acquisition Via Full And Open Competition. Only The Source(s) Previously Approved By The Government For This Item Have Been Solicited. The Time Required For Approval Of A New Source Is Normally Such That An Award Cannot Be Delayed Pending Approval Of A New Source. If You Are Not An Approved Source You Must Submit, Together With Your Proposal, The Information Detailed In One Of The Navsup Weapon Systems Support (navsup Wss) Source Approval Information Brochures Listed Below. Spares: Https://www.navsup.navy.mil/navsup-enterprise/navsup-weapon-systems-sup Port/business-opps/ Repair: Https://www.navsup.navy.mil/navsup-enterprise/navsup -weapon-systems-support/business-opps/ Technical Data Required To Be Submitted Based On Your Company's Experience In Production Of The Same Or Similar Item, Or If This Is An Item You Have Never Made. If Your Request For Source Approval Is Currently Being Evaluated At Navsup Wss Submit With Your Offer A Copy Of The Cover Letter Which Forwarded Your Request For Source Approval. Offers Received Which Fail To Provide All Data Required By The Source Approval Brochure Or Document Previous Submission Of All Data Required By The Source Approval Brochure Will Not Be Considered For Award Under This Solicitation. Please Note, If Evaluation Of A Source Approval Request Submitted Hereunder Cannot Be Processed In Time And/or Approval Requirements Preclude The Ability To Obtain Subject Items In Time To Meet Government Requirements, Award Of The Subject Requirement May Continue Based On Fleet Support Needs. The Navsup Wss Commercial Item Identification Brochure Is Now Available At: "https://www.navsup.navy.mil/navsup-enterprise/navsup-weapon-systems-support/bus Iness-opps/" Interested Parties May Obtain Copies Of Military And Federal Specificationsand Standards, Qualified Products Lists (qpls), Qualified Product Databases(qpds), Military Handbooks, And Other Standardized Documents From The Dodsingle Stock Point (dodssp) At Document Automation And Production Service(daps) In Philadelphia, Pa. Note: Patterns, Drawings, Deviation Lists, Purchase Descriptions, Etc. Are Not Stocked At Dodssp. Most Documents Are Available In Adobe Pdf Format From Assist-online At: Http://quicksearch.dla.mil/. Users May Use Assist-quick Search To Search For And Download Available Documents Directly Using Standard Browser Software. Documents That Are Not Available For Downloading From Assist-quick Search Can Be Ordered From The Dodssp Website Using The Assist Shopping Wizard After Obtaining A Dodssp Customer Account By Following The Registration Procedures. Users Who Do Not Have Access To The Internet May Contact The Dodssp Assisthelp Desk At 215-697-2667 Or 215-697-2179 (dsn: 442-2667), Or Mail Their Request To Dladocument Services, Bldg. 4/d, 700 Robbins Avenue, Philadelphia Pa 19111-5094. The Proposed Contract Action Is For Supplies Or Services For Which The Government Intends To Solicit And Negotiate With Only One Source Under The Authority Of Far 6.302-1. All Responsible Sources May Identify Their Interest And Capability To Respond To The Requirement Or Submit Proposals, Quotationsor Capability Statements. This Notice Of Intent Is Not A Request Forcompetitive Proposals. However, All Proposals Received Within 45 Days (30days If Award Is Issued Under An Existing Basic Ordering Agreement (boa) Afterdate Of Publication Of This Synopsis Will Be Considered By The Government. A Determination By The Government Not To Compete With This Proposed Contract Based Upon Responses To This Notice Is Solely Within The Discretion Of The Government. Information Received Will Normally Be Considered Solely For The Purpose Of Determining Whether To Conduct A Competitive Procurement.

Details: This Is A Modification 6 To The Synopsis Entitled Extravehicular Activity And Human Surface Mobility Technologies, Reference No. 80jsc022ehp Which Was Posted On September 23, 2022. You Are Notified That The Following Changes Are Made: purpose: extended The Response Date From 1/16/2025 To 1/16/2027. the Due Date For Responses Is Extended. offerors Are Responsible For Monitoring This Site For The Release Of The Solicitation And Any Amendments. Potential Offerors Are Responsible For Downloading Their Own Copy Of The Solicitation And Amendments. ***end Of Modification 6*** this Is A Modification 5 To The Synopsis Entitled Extravehicular Activity And Human Surface Mobility Technologies, Reference No. 80jsc022ehp Which Was Posted On September 23, 2022. You Are Notified That The Following Changes Are Made: purpose: this Is A Modification 5 To Update The Point Of Contact (poc) From: contact Information: technology Development And Partnerships Manager, eva & Human Surface Mobility Program email: Michael.a.berdich@nasa.gov to: contact Information: technology Development And Partnerships Manager, eva & Human Surface Mobility Program email: Stephanie.a.sipila@nasa.gov the Due Date For Responses Is Not Extended. offerors Are Responsible For Monitoring This Site For The Release Of The Solicitation And Any Amendments. Potential Offerors Are Responsible For Downloading Their Own Copy Of The Solicitation And Amendments. ***end Of Modification 5*** this Is A Modification 4 To The Synopsis Entitled Extravehicular Activity And Human Surface Mobility Technologies, Reference No. 80jsc022ehp Which Was Posted On September 23, 2022. You Are Notified That The Following Changes Are Made: correct The Modification 3 revise The Entry Titled “modification 2” To Reflect It As “modification 1.” Additionally, Incorporate Relevant Links In Bold Into This Entry. the Following Link Https://nasajsc.secure.force.com/statementofinterest Is No Longer Valid Please Refer To The Link Below Titled: The Statement Of Interest In The Attachments/links Section. purpose: the Nasa Extravehicular Activity (eva) And Human Surface Mobility (hsm) Program (ehp) Seeks To Work With Partners To Advance The Technologies Associated With Human Surface Mobility In Support Of Nasa’s Artemis Missions. The Ehp Vision Is To Provide Safe, Reliable, And Effective Eva And Hsm Capabilities That Allow Astronauts To Survive And Work Outside The Confines Of A Spacecraft On And Around The Moon. Artemis Missions Will Return Humans To The Surface Of The Moon Using Innovative Technologies To Explore More Of The Lunar Surface Than Ever Before. We Will Collaborate With Commercial And International Partners And Establish The First Long-term Presence On The Moon. Then, We Will Use What We Learn On And Around The Moon To Take The Next Giant Leap: Sending The First Astronauts To Mars. ehp Flight Projects Are Exploration Eva Suits (xeva Suits) And Tools, Lunar Terrain Vehicle (ltv), And Pressurized Rover (pr). For More Information, Reference The Ehp Website Here: Extravehicular Activity And Human Surface Mobility - Nasa (https://www.nasa.gov/extravehicular-activity-and-human-surface-mobility/). the Ehp And Partners Will Collaborate On Developing Lunar Surface Capabilities To Reduce Risk And Increase Productivity Of Ehp Flight Projects During Artemis Missions. Focus Will Be On Technologies That Mitigate Risk For Lunar Surface Systems That Will Provide Mission Planners With More Choices, Thereby Increasing Mission Success. In Pursuing These Types Of Capabilities, Nasa And Potential Partners Will Develop New And Improved Technologies That Will Provide Additional Options For Terrestrial Applications In Multiple Industries. additional Information: ehp May Periodically Publish In Appendices To This Announcement Identifying Specific Technologies Under Current Development To Further Inform Potential Collaboration Opportunities. An Example Of One Such Technology Being Developed Is Described In Appendix A - Lunar Dust Level Sensor And Effects On Surfaces (ldes). For Access To This Export-controlled Document, Please Email The Points Of Contact Below. ehp Periodically Places Informational Reference Documents That Relate To Lunar Human Surface Mobility Accessible By Industry In The Ehp Technical Library (https://eva.jsc.nasa.gov/). Access To The Technical Library Requires Login.gov Access. Follow The Prompts To Gain Access. Once Access Has Been Granted, The Informational Documents Related To This Announcement Is In The ‘ehp Technology Integration’ Folder, In Which You Will Find Information On The Following (major Updates To The Technical Library Content Will Also Be Updated Here): - Ldes – Initial Ground Test Results Regarding The Magnitude Of Thermal Impact That Lunar Dust Has On Surfaces. - 84s Lunar Terrain Model – A Terrain Model Of The Lunar South Pole (below The 84 South Latitude) Which Can Be Used As An Early Reference Data Set To Enable Initial Studies Of The Lunar Terrain. additionally, Nasa Has Made Available To The Public The Digital Lunar Exploration Sites Unreal Simulation Tool (dust) Which Is An Early 3d Visualization Application Of The Lunar South Pole. Its Intended Use Is For Early Inspection, Mission Planning, And Analysis Of Lunar Landing And Traverse Sites For Hls And Artemis Base Camp. This Application And The Supporting Toolkit Built From Dust Are Used To Provide Distributable Lunar Environments And Tools To Support Rendering And Exporting Terrain, Multi-display Facilities, And Connections To Trick-based Simulations. It Can Be Attained At The Following Link: Digital Lunar Exploration Sites Unreal Simulation Tool (dust) Products(msc-27522-1) | Nasa Software Catalog (https://software.nasa.gov/software/msc-27522-1). technology: ehp Technology Goals Include, But Are Not Limited To, Overcoming Environmental And Long Mission Duration Challenges. Lunar Environmental Challenges Include Operating In Dust (lunar Regolith), Radiation, And Extreme Temperatures. Martian Environmental Challenges Are Operating In Martian Carbon Dioxide-rich Atmosphere And 1/3g, Driving The Need For Low Size, Weight, And Power. Long Mission Durations Drive Sustainability And Maintainability Challenges. Some Technology Areas Of Interest Include, But Are Not Limited To: Dust Mitigation Capabilities, Eva Systems, Local Relative Navigation, Increased Battery Capacity And Reduced Charge Time, And Advanced Mobility Concepts Capable Of Sustained Operation While Minimizing Maintenance In A Lunar Environment For An Extended Service Period. Each System Will Be Required To Operate In The Extreme Environment Of Cis-lunar Orbit And/or The Lunar South Pole, Including Inside Permanently Shadowed Regions (psrs) And Onto Mars. intellectual Property (ip): this Potential Partnership May Produce New Ip That Could Be Jointly Owned By Nasa And The Partner Or May Become The Property Of The Partner. Standard Clauses For Partnership Agreements Are Provided In The Appendices Of The Space Act Agreements Guide, Naii 1050-1. These Standard Clauses Are Usually Used Without Any Changes. Any Deviations From The Standard Intellectual Property Clauses Are Reviewed By Nasa Office Of The General Counsel At The Headquarters And/or Center-level, As Appropriate And Approved By Nasa Partnerships Office. potential Commercial Applications: lunar, Undersea, Automotive, Nuclear, Space Tourism, Personal Protective Equipment (ppe) … keywords: mobility, Spacesuit, Rover, Vehicle, Power Infrastructure, Sustainable, Dust, Communication Architecture, Relative Navigation And Localization, Regolith, Lunar Terrain Vehicle, Ltv, Pressurized Rover, Pr, Lunar, Artemis, Moon, Iss, Leo contact Information: technology Development And Partnerships Manager, eva & Human Surface Mobility Program email: Michael.a.berdich@nasa.gov partnership Manager, jsc’s Partnership Development Office email: Jsc-partnerships@mail.nasa.gov to Respond To This Announcement, Please Use The Statement Of Interest Form Found At statement Of Interest (https://docs.google.com/forms/d/e/1faipqlsclwzeqitigc1wauvfvegkykseuozom0uofxtc60gk_giretq/viewform?usp=sharing) to View All Co-development And Partnering Opportunities With The Nasa Johnson Space Center, Please Visit Our Website At (https://www.nasa.gov/johnson/exploration/technology/co-development-and-partnering-opportunities) the Due Date For Responses Is Not Extended. offerors Are Responsible For Monitoring This Site For The Release Of The Solicitation And Any Amendments. Potential Offerors Are Responsible For Downloading Their Own Copy Of The Solicitation And Amendments. ***end Of Modification 4*** this Is A Modification 3 To The Synopsis Entitled Extravehicular Activity And Human Surface Mobility Technologies, Reference No. 80jsc022ehp Which Was Posted On September 23, 2022. You Are Notified That The Following Changes Are Made: update Modifcation 2 In Its Entirety: purpose: the Nasa Extravehicular Activity (eva) And Human Surface Mobility (hsm) Program (ehp) Seeks To Work With Partners To Advance The Technologies Associated With Human Surface Mobility In Support Of Nasa’s Artemis Missions. The Ehp Vision Is To Provide Safe, Reliable, And Effective Eva And Hsm Capabilities That Allow Astronauts To Survive And Work Outside The Confines Of A Spacecraft On And Around The Moon. Artemis Missions Will Return Humans To The Surface Of The Moon Using Innovative Technologies To Explore More Of The Lunar Surface Than Ever Before. We Will Collaborate With Commercial And International Partners And Establish The First Long-term Presence On The Moon. Then, We Will Use What We Learn On And Around The Moon To Take The Next Giant Leap: Sending The First Astronauts To Mars. ehp Flight Projects Are Exploration Eva Suits (xeva Suits) And Tools, Lunar Terrain Vehicle (ltv), And Pressurized Rover (pr). For More Information, Reference The Ehp Website Here: Extravehicular Activity And Human Surface Mobility - Nasa the Ehp And Partners Will Collaborate On Developing Lunar Surface Capabilities To Reduce Risk And Increase Productivity Of Ehp Flight Projects During Artemis Missions. Focus Will Be On Technologies That Mitigate Risk For Lunar Surface Systems That Will Provide Mission Planners With More Choices, Thereby Increasing Mission Success. In Pursuing These Types Of Capabilities, Nasa And Potential Partners Will Develop New And Improved Technologies That Will Provide Additional Options For Terrestrial Applications In Multiple Industries. additional Information: ehp May Periodically Publish In Appendices To This Announcement Identifying Specific Technologies Under Current Development To Further Inform Potential Collaboration Opportunities. An Example Of One Such Technology Being Developed Is Described In Appendix A - Lunar Dust Level Sensor And Effects On Surfaces (ldes). For Access To This Export Controlled Document, Please Email The Points Of Contact Below. ehp Periodically Places Informational Reference Documents That Relate To Lunar Human Surface Mobility Accessible By Industry In The Ehp Technical Library. Access To The Technical Library Requires Login.gov Access. Follow The Prompts To Gain Access. Once Access Has Been Granted, The Informational Documents Related To This Announcement Is In The ‘ehp Technology Integration’ Folder, In Which You Will Find Information On The Following (major Updates To The Technical Library Content Will Also Be Updated Here): ldes – Initial Ground Test Results Regarding The Magnitude Of Thermal Impact That Lunar Dust Has On Surfaces. 84s Lunar Terrain Model – A Terrain Model Of The Lunar South Pole (below The 84 South Latitude) Which Can Be Used As An Early Reference Data Set To Enable Initial Studies Of The Lunar Terrain. additionally, Nasa Has Made Available To The Public The Digital Lunar Exploration Sites Unreal Simulation Tool (dust) Which Is An Early 3d Visualization Application Of The Lunar South Pole. Its Intended Use Is For Early Inspection, Mission Planning, And Analysis Of Lunar Landing And Traverse Sites For Hls And Artemis Base Camp. This Application And The Supporting Toolkit Built From Dust Are Used To Provide Distributable Lunar Environments And Tools To Support Rendering And Exporting Terrain, Multi-display Facilities, And Connections To Trick-based Simulations. It Can Be Attained At The Following Link: Digital Lunar Exploration Sites Unreal Simulation Tool (dust) Products(msc-27522-1) | Nasa Software Catalog. technology: ehp Technology Goals Include, But Are Not Limited To, Overcoming Environmental And Long Mission Duration Challenges. Lunar Environmental Challenges Include Operating In Dust (lunar Regolith), Radiation, And Extreme Temperatures. Martian Environmental Challenges Are Operating In Martian Carbon Dioxide-rich Atmosphere And 1/3g, Driving The Need For Low Size, Weight, And Power. Long Mission Durations Drive Sustainability And Maintainability Challenges. Some Technology Areas Of Interest Include, But Are Not Limited To: Dust Mitigation Capabilities, Eva Systems, Local Relative Navigation, Increased Battery Capacity And Reduced Charge Time, And Advanced Mobility Concepts Capable Of Sustained Operation While Minimizing Maintenance In A Lunar Environment For An Extended Service Period. Each System Will Be Required To Operate In The Extreme Environment Of Cis-lunar Orbit And/or The Lunar South Pole, Including Inside Permanently Shadowed Regions (psrs) And Onto Mars. intellectual Property (ip): this Potential Partnership May Produce New Ip That Could Be Jointly Owned By Nasa And The Partner Or May Become The Property Of The Partner. Standard Clauses For Partnership Agreements Are Provided In The Appendices Of The Space Act Agreements Guide, Naii 1050-1. These Standard Clauses Are Usually Used Without Any Changes. Any Deviations From The Standard Intellectual Property Clauses Are Reviewed By Nasa Office Of The General Counsel At The Headquarters And/or Center-level, As Appropriate And Approved By Nasa Partnerships Office. potential Commercial Applications: lunar, Undersea, Automotive, Nuclear, Space Tourism, Personal Protective Equipment (ppe) … keywords: mobility, Spacesuit, Rover, Vehicle, Power Infrastructure, Sustainable, Dust, Communication Architecture, Relative Navigation And Localization, Regolith, Lunar Terrain Vehicle, Ltv, Pressurized Rover, Pr, Lunar, Artemis, Moon, Iss, Leo contact Information: technology Development And Partnerships Manager, eva & Human Surface Mobility Program email: Michael.a.berdich@nasa.gov partnership Manager, jsc’s Partnership Development Office email: Jsc-partnerships@mail.nasa.gov to Respond To This Announcement, Please Use The Statement Of Interest Form Found At statementofinterest to View All Co-development And Partnering Opportunities With The Nasa Johnson Space Center, Please Visit Our Website At https://www.nasa.gov/johnson/exploration/technology/co-development-and-partnering-opportunities extended The Response Date From 9/26/2024 To 1/16/2025 the Due Date For Responses Is Extended. offerors Are Responsible For Monitoring This Site For The Release Of The Solicitation And Any Amendments. Potential Offerors Are Responsible For Downloading Their Own Copy Of The Solicitation And Amendments. ***** End Of Modification 3**** this Is A Modification 2 To The Synopsis Entitled Extravehicular Activity And Human Surface Mobility Technologies, Reference No. 80jsc022ehp Which Was Posted On September 23, 2022. You Are Notified That The Following Changes Are Made: extended The Response Date From 9/26/2023 To 9/26/2024 the Due Date For Responses Is Extended. offerors Are Responsible For Monitoring This Site For The Release Of The Solicitation And Any Amendments. Potential Offerors Are Responsible For Downloading Their Own Copy Of The Solicitation And Amendments. *****end Of Modiffication 2 ****** this Is A Modification 1 To The Synopsis Entitled Extravehicular Activity And Human Surface Mobility Technologies, Reference No. 80jsc022ehp Which Was Posted On September 23, 2022. You Are Notified That The Following Changes Are Made: new Attachment: Appendix A – Lunar Dust Level Sensor And Effects On Surfaces new Purpose Statement Added In Bold. the Due Date For Responses Is Not Extended. offerors Are Responsible For Monitoring This Site For The Release Of Any New Special Notice. purpose: the Nasa Extravehicular Activity (eva) And Human Surface Mobility (hsm) Program (ehp) Seeks To Work With Partners To Advance The Technologies Associated With Human Mobility And Lunar Surface Infrastructure In Support Of Nasa’s Artemis Missions. The Ehp Vision Is To Provide Safe, Reliable, And Effective Eva And Hsm Capabilities That Allow Astronauts To Survive And Work Outside The Confines Of A Spacecraft On And Around The Moon. Artemis Missions Will Return Humans To The Surface Of The Moon Using Innovative Technologies To Explore More Of The Lunar Surface Than Ever Before. We Will Collaborate With Commercial And International Partners And Establish The First Long-term Presence On The Moon. Then, We Will Use What We Learn On And Around The Moon To Take The Next Giant Leap: Sending The First Astronauts To Mars. the Ehp And Partners Will Collaborate On Developing Lunar Capabilities To Increase Productivity Of Relevant Systems Allowing Crew To Accomplish More During Artemis Missions. Focus Will Be On High-risk Technologies For Lunar Surface Systems That Will Provide Mission Planners With More Choices, Thereby Increasing Mission Success. In Pursuing These Types Of Capabilities, Nasa And Potential Partners Will Develop New And Improved Technologies That Will Provide Additional Options For Terrestrial Applications In Multiple Industries. ehp May Periodically Publish In Appendices To This Announcement Identifying Specific Technologies Under Current Development To Further Inform Potential Collaboration Opportunities. An Example Of One Such Technology Being Developed Is Described In Appendix A - Lunar Dust Level Sensor And Effects On Surfaces (ldes).for Access To This Export Controlled Document, Please Email The Points Of Contact Below. technology: technology Goals Include, But Are Not Limited To: Dust Mitigation Capabilities, Eva Systems, Lunar Power And Communication Infrastructure, Local Relative Navigation, Increased Battery Capacity And Reduced Charge Time, And Advanced Mobility Concepts Capable Of Sustained Operation While Minimizing Maintenance In A Lunar Environment For An Extended Service Period. Each System Will Be Required To Operate In The Extreme Environment Of Cis-lunar Orbit And/or The Lunar South Pole, Including Inside Permanently Shadowed Regions (psrs) And Onto Mars. intellectual Property (ip): this Potential Partnership May Produce New Ip That Could Be Jointly Owned By Nasa And The Partner Or May Become The Property Of The Partner. Standard Clauses For Partnership Agreements Are Provided In The Appendices Of The Space Act Agreements Guide, Naii 1050-1. These Standard Clauses Are Usually Used Without Any Changes. Any Deviations From The Standard Intellectual Property Clauses Are Reviewed By Nasa Office Of The General Counsel At The Headquarters And/or Center-level, As Appropriate And Approved By Nasa Partnerships Office. potential Commercial Applications: lunar, Undersea, Automotive, Nuclear, Space Tourism, Personal Protective Equipment (ppe) … keywords: mobility, Spacesuit, Rover, Vehicle, Power Infrastructure, Sustainable, Dust, Communication Architecture, Relative Navigation And Localization, Regolith, Lunar Terrain Vehicle, Ltv, Pressurized Rover, Pr, Lunar, Artemis, Moon, Iss, Leo to Respond To This Announcement, Please Use The Statement Of Interest Form Found At The Link Below. to View All Co-development And Partnering Opportunities With The Nasa Johnson Space Center, Please Visit Our Website At https://www.nasa.gov/johnson/exploration/technology/co-development-and-partnering-opportunities

Details: On-site and remote preventive and corrective maintenance of pneumatic transport networks of the Aerocom and Elektror brands and updating of associated software

Details: The National Aeronautics And Space Administration (nasa) Langley Research Center (larc) Is In The Early Stages Of Developing A Mission Design, Project Implementation Plan, And Procurement Strategy That Could Potentially Lead To An Earth Aerocapture Technology Demonstration Mission. Nasa Larc Is Hereby Soliciting Information From Potential Sources With The Capabilities To Provide Spacecraft Systems And Mission Operations For The Mission. the Mission Would Demonstrate Aerocapture At Earth As A Precursor To Using The Technology For Future Planetary Science Missions. Aerocapture Technology Reduces The Required Capability And Mass Of A Spacecraft Propulsion System, Lowering The Launch Vehicle Payload Mass Or Enabling More Capacity For Science Instruments, And Is Particularly Beneficial For Missions To The Solar System's Ice Giant Planets [1]. The Demonstration Mission Is Intended To Focus On Key Objectives Necessary To Mature The Technological Readiness Of Aerocapture Including Vehicle Aerodynamics, Flight Dynamics, Guidance, Navigation And Control, And Mission Operations. Flight Data Will Be Acquired During The Demonstration And Used To Improve And Validate Tools To Design And Plan Future Missions. nasa Is Considering Two Concepts For The Mission, Both Of Which Use A Small Entry Capsule (referred To As The Aerocapture Flight System, Or Afs) To Execute The Aerocapture Maneuver. The Afs Is Comprised Of An Aeroshell, Reaction Control System, Other Ancillary Systems, And A Smallsat That Is Released Into Earth Orbit. The First Mission Concept Utilizes A Geostationary Transfer Orbit (gto) As An Initial State For The Afs, Which Is Deployed Into Gto From An Evolved Expendable Launch Vehicle (eelv) Secondary Payload Adapter (espa). In The Second Concept, The Afs Is Released On An Earth Intercept Trajectory From A Spacecraft Returning From A Lunar Mission. A Preliminary Concept Of Operations (conops) For A Gto-based Aerocapture Demonstration Is Illustrated In Figure 1 (attached). Details Shown Regarding Orbit Altitudes Are For Reference Only, And Will Continue To Be Resolved (tbr) In Upcoming Design Trades. referring To Figure 1, The Preliminary High-level Mission Conops And Sequence Of Events Is As Follows. The Sequence Of Events Is For Reference And Context Only To Support The Vendors' Responses To This Request For Information, And Will Continue To Be Updated As Nasa Larc Progresses Through The Early Stages Of Mission Design. the Afs, Attached To The Port Of An Espa Grande With A Separation Mechanism, Is Delivered And Released Into Gto By The Launch Vehicle. The Afs Continues In Gto While Using Its Reaction Control System To Maintain Attitude During Preparations For The Aerocapture Maneuver. Nasa's Intention Is For The Afs To Complete Less Than Two Full Orbits Before Beginning The Aerocapture Maneuver. near Gto Apogee, The Afs Reaction Control System Delivers The Delta-v Required To Divert The Capsule Along The Flight Path Necessary To Intercept The Earth's Atmosphere And Initialize The Aerocapture Maneuver. the Afs Reaction Control System Continually Adjusts The Capsule's Attitude, Utilizing The Vehicle's Aerodynamic Lift To Maintain Its Flight Path Inside A Pre-planned Corridor Through The Earth's Atmosphere With A Periapsis Of Approximately 65 Km (tbr). after Completing The Atmospheric Flight, The Afs Exits The Earth's Atmosphere In An Elliptical Orbit With An Apoapsis Of Approximately 500 Km (tbr). within 15 Minutes (tbr) After Exiting The Earth's Atmosphere, The Forward Heatshield Of The Afs Aeroshell Is Jettisoned And A Smallsat Is Released Into The New Elliptical Orbit. The Smallsat Utilizes Its Attitude Control System To Attain A Stable Attitude And Prepares For An Apogee Burn To Circularize The Orbit. when The Smallsat Reaches Apogee For The First Time, Its Propulsion System Delivers The Delta-v Necessary To Circularize The Orbit At An Altitude Of 500 Km (tbr). the Smallsat Continues In Its Circular Orbit Until The Flight Data Acquired Throughout The Demonstration Has Been Transmitted To Ground Stations. Successful Transmission Of The Flight Data Signifies The End Of The Demonstration, Subject To Any Spacecraft Disposal Operations Necessary In Accordance With Nasa Orbital Debris Requirements [2, 3]. the Salient Features And High-level Functional Requirements Of The Afs That Are Envisioned To Support The Mission’s Preliminary Concept Of Operations Are As Follows. Since Nasa Is In The Early Stages Of Mission And System Design, These Features And Requirements Are Subject To Change As The Design Matures. The Information Is Provided Herein As A Reference For Vendors To Consider When Evaluating The Mission Concept And Assessing The Capabilities That Vendors May Contribute To The Demonstration Mission In Response To This Request For Information. afs Mass And Volume: The Afs Shall Be A Blunt-body Capsule With A 60° (tbr) Sphere-cone Forebody Geometry. The Aeroshell Backshell Geometry Has Not Been Determined, But Must Provide The Volume To Accommodate The Smallsat, The Afs Reaction Control System, Wiring Harnesses, And Ancillary Systems Required To Perform The Mission. The Afs Shall Possess The Mass And Volume To Be Accommodated On A Single Port Of An Espa Grande [4]. afs Aeroshell: The Aeroshell Shall Be Comprised Of A Forebody Heatshield Structure And A Backshell Structure With Mechanical Provisions To Separate The Two Structures After Completion Of The Aerocapture Maneuver. The Backshell Structure Shall Accommodate A Separation Ring To Attach And Release The Afs From The Espa Grande Port. Either Structure Shall Incorporate The Mechanical Interface To Attach And Release The Smallsat After The Aeroshell Structures Are Separated. The Backshell Shall Incorporate External Mechanical Interfaces For Ground Support Equipment (gse) And Electrical Connections For Battery Charging And Functional Tests Prior To Launch. Devices To Sever Wiring Harnesses Between The Smallsat And Afs Systems Will Be Required, And Depending On The Smallsat's Telecommunications Configuration, An Antenna(s) Mounted To The Backshell Structure May Also Be Needed. aerodynamic Lift Provisions: The Afs Will Control Its Flight Path During The Aerocapture Maneuver By Modulating The Magnitude And/or Direction Of The Entry Capsule's Aerodynamic Lift Vector (e.g., Bank Angle Modulation). The Vehicle's Aerodynamic Lift Is Envisioned To Be Produced By The Capsule Flying At An Angle-of-attack Induced By Either A Center-of-gravity (cg) Offset Or An Asymmetric Aerodynamic Device Such As A Trim Tab. Nasa's Near-term Trade Studies Will Evaluate The Different Methods Of Producing Aerodynamic Lift Considering System Mass, Technological Readiness, Complexity, And Risk. thermal Protection Systems: The Aeroshell Forebody Heatshield And Backshell Shall Include Government-furnished Thermal Protection Systems (tps) To Protect The Afs From The Aerothermal Environments Produced During The Aerocapture Maneuver. The Tps Will Be Designed To Accommodate The Entry System Instrumentation (esi) Described Below And Other Ancillary Systems And Interfaces That Require Tps Penetrations For Installation And/or Operation. entry System Instrumentation: The Government Will Furnish Esi To Be Incorporated Into The Aeroshell Heatshield And Backshell. The Esi Will Be Comprised Of Thermocouples And Pressure Transducers, The Quantities And Locations Of Which Have Not Been Determined, To Measure The Afs Entry Environments During The Aerocapture Maneuver. A Flight Data System Residing On The Smallsat Shall Provide Power To The Esi And Record And Store The Esi Data That Will Be Transmitted To Ground Stations Near The Conclusion Of The Demonstration. afs Reaction Control System: The Afs Shall Incorporate A Reaction Control System With The Capability To Correct For Launch Vehicle Orbit Insertion Dispersions, Deliver The Delta-v To Divert The Afs Into The Intended Earth Atmosphere Interface Conditions For Aerocapture, And Maintain Afs Attitude As Required From Gto Insertion Through The Aerocapture Maneuver To The Point When The Aeroshell Separates And The Smallsat Is Released. afs Smallsat: The Preliminary Demonstration Mission Concept Of Operations Requires The Afs Smallsat To Be Operational For The Full Duration Of The Technology Demonstration Timeline. The Smallsat Shall Provide Power, Avionics And Flight Instrumentation Including An Inertial Measurement Unit (imu), Command And Data Handling (c&dh), Attitude Determination And Control, And Communications For All Mission Phases From Gto Insertion To Data Download And Orbital Debris Mitigation (as Required). The Smallsat Is Required To Interface With External Systems, Such As The Afs Reaction Control System And Esi, To Support The Mission Through The Aerocapture Maneuver, And Then Operate In A Stand-alone Configuration After Being Released From The Aeroshell. to Aid In Continuing The Formulation Of A Mission Design And Developing A Procurement Strategy To Implement The Mission, Nasa Larc Is Conducting Market Research Seeking Sources With Demonstrated Experience To Provide The Following Capabilities To Support The Demonstration Mission. design And Delivery Of The Afs: Design, Fabricate, Integrate, And Test The Afs Including The Aeroshell, Reaction Control System, Smallsat, Separation Systems, And Government-furnished Tps And Esi. Deliver The Afs To The Launch Provider And Support Assembly, Test, And Launch Operations (atlo). mission Design And Navigation: Design Of The Orbital Mechanics And Navigation From The Point The Afs Is Released Into Gto To End-of-mission. Mission Design Will Be Supplemented By Government-furnished Guidance, Navigation And Control (gnc) Software To Control The Afs During The Aerocapture Maneuver. Capabilities Shall Include Experience With Mission Design And Navigation For High-energy Earth Orbits And Missions Returning From Lunar Environs. mission Operations: Establish A Ground Operating System And Conduct Mission Operations For All Phases Of The Demonstration From Launch To Mission Termination. nasa Larc Is Seeking Capability Statements From All Interested Parties, Including All Socioeconomic Categories Of Small Businesses And Historically Black Colleges And Universities (hbcu)/minority Institutions (mi), And Members Of The Underserved Communities As Defined By Executive Order 13985, Advancing Racial Equity And Support For Underserved Communities Through The Federal Government, For The Purposes Of Determining The Appropriate Level Of Competition And/or Small Business Subcontracting Goals For The Earth Aerocapture Technology Demonstration Mission. The Government Reserves The Right To Consider A Small, 8(a), Women-owned (wosb), Service Disabled Veteran (sd-vosb), Economically Disadvantaged Women-owned Small Business (edwosb) Or Hubzone Business Set-aside Based On Responses Received. no Solicitation Exists; Therefore, Do Not Request A Copy Of The Solicitation. If A Solicitation Is Released, It Will Be Synopsized On Sam.gov. Interested Firms Are Responsible For Monitoring This Website For The Release Of Any Solicitation Or Synopsis. interested Firms Possessing One Or More Of The Capabilities Described Above Should Submit A Capability Statement Of No More Than 20 Pages(excluding Cover Page And Table Of Contents) Indicating The Ability To Perform These Aspects Of The Demonstration Mission. Please Include The Following Elements In The Capability Statement. mission Conops Assessment: The Preliminary Mission Conops Described Herein Was Formulated To Advance The Technology Readiness Level (trl) Of Aerocapture And Enable Its Infusion Into Future Planetary Missions. The Conops Includes Multiple Events Requiring Mechanical Separations And Severing Of Wiring Harnesses, And Relies On A Smallsat Capable Of Controlling A Flight System In Two Different Configurations (afs And Stand-alone Smallsat). Provide An Assessment Of The Preliminary Conops Identifying Design Drivers And Risks Relative To Existing State-of-the-art Systems And Your Capabilities And Experience. Please Include An Evaluation Of The Potential Mass And Volume Of The Afs Relative To The Espa Grande Accommodation Requirements. Suggest Changes In The Conops Or The Afs Configuration That Would Substantially Reduce Risk And Cost Without Significantly Compromising The Demonstration Objectives. describe Your Organization's Capability And Experience To Provide A Smallsat Spacecraft And Flight Software That Meets The Mission Requirements. Due To The Anticipated Fast-paced Implementation Of The Mission, Smallsats That Are Nearly "off-the-shelf" Are Considered To Be Advantageous To Mission Success. Include Information On The Smallsat Form Factor, Mass, Accommodation Requirements, And Operational Heritage. Describe The Smallsat Capability To Interface And Manage External Systems Such As The Afs Reaction Control System, And Explain How The Smallsat Would Accommodate The Changes In The Flight System Configuration That Occur During The Mission. describe Your Organization's Capability And Experience To Design And Provide The Afs Aeroshell. Provide Examples Of Aeroshells Of Similar Scale And Mass Utilized For Earth Atmospheric Entry In Previous Missions. Describe The Basic Aeroshell Structural Architecture And Any Unique Features Required By The Mission That Introduce Substantial Risk And Cost. Discuss The Provisions Necessary To Implement The Three Separation Events Required For The Mission Conops: 1) Separation Of The Afs From The Espa Grande, 2) Separation Of The Afs Forebody Heatshield, And 3) Separation Of The Smallsat From The Aeroshell. describe Your Organization's Capability And Experience To Plan And Conduct The Afs Integration And Testing. Include A Description Of Facilities, Ground Support Equipment, And Capabilities For Afs Environmental Testing. Include A Description Of Previous Experience Integrating Thermal Protection Systems Onto Blunt-body Aeroshells And The Installation Of Thermocouple And Pressure Transducer Instrumentation. describe Your Organization's Capability And Experience To Design Missions And Navigation Strategies For Spacecraft In High-energy Earth Orbits Or Returning From The Moon. Include Information On Analysis Tools And Methods And Highlight Any Previous Missions With A Concept Of Operations Similar To The Aerocapture Demonstration Mission. describe Your Organization's Capability To Establish A Ground Operating System And Conduct Mission Operations. Include Information On Existing Infrastructure That Would Be Leveraged For The Mission Including Telecommunications Ground Stations, Mission Operating Centers, And Ancillary Hardware And Software. describe Your Plans For Partnering With Other Organizations To Provide Any Of The Aforementioned Capabilities For The Mission. all Responses Shall Be Submitted Electronically Via Nasa’s Enterprise File Sharing And Sync Box (efss Box), Fedramp Moderate Certified Platform, No Later Than January 15, 2025. Electronic Submissions Shall Not Contain Hidden Formulas, Tables, Be Locked, Be Password Protected, Or Contain Links To Data Not Included In The Electronic Copy. Please Reference The Synopsis Number And “earth Aerocapture Demonstration Rfi” In Any Response. All Responses Shall Be Submitted To: Https://nasagov.app.box.com/f/7cf6c2fec43e4f7b8d1dff31208c6be9. If You Have Any Trouble Submitting Your Response Via Efss Box, Please Contact Stacy Hollis At Stacy.m.hollis@nasa.gov. this Synopsis Is For Information And Planning Purposes Only And Is Not To Be Construed As A Commitment By The Government Nor Will The Government Pay For Information Solicited. Respondents Will Not Be Notified Of The Results Of The Evaluation. references: [1] "uranus Flagship-class Orbiter And Probe Using Aerocapture," Aiaa 2024-0714, Aiaa Scitech Forum, Orlando, Florida, January 2024. [2] "process For Limiting Orbital Debris," Nasa-std-8719.14c , November 5, 2021. [3] "orbital Debris Mitigation," Nasa-npr-8715.6e, April 18, 2024. [4] "espa User's Guide, The Eelv Secondary Payload Adapter," Moog, Incorporated.

Details: General Procurement Notice (gpn) Country : The People’s Republic Of Bangladesh Name Of Project : Rural And Peri-urban Housing Finance Project-second Phase Executing Agency (ea) : Bangladesh House Building Finance Corporation (bhbfc) Mode Of Financing : Installment Sale Financing And Ocr Loan Financing No : Bgd-1087 The Government Of The People’s Republic Of Bangladesh Has Applied For Financing In The Amount Of Euro 270.57 Million Equivalent From The Islamic Development Bank (isdb) Towards The Cost Of The Rural And Peri-urban Housing Financing Project-second Phase In Bangladesh And It Intends To Apply Part Of The Proceeds To Payments For Goods, Works, Related Services And Consulting Services To Be Procured Under This Project. This Project Will Be Jointly Financed By The Islamic Development Bank (isdb) And Government Of Bangladesh (gob)/bhbfc. The Project Will Include The Following Components: Component-a Financing For Construction Of Houses/building With Related Facilities: This Is The Main Component Of The Project, Mainly Financing For The Construction Of Multi-story Buildings In Project Areas. The Said Financing Will Ensure The Development Of Sufficient Numbers Of Planned And Affordable Houses With Improved Basic Facilities (water Supply, Sanitation Facilities And Electricity). It Will Also Lead A Participation Of Country’s Effort In Reduction Of Greenhouse Gas (ghg) Emissions Through The Financing To Eco-friendly And Climate Resilient Housing. Component-b Capacity Development Program For Developing Housing Models And Related Financing: This Component Will Finance For The Recruitment Of Consultants For Developing Convenient Housing Models Under And In Line With Project Objectives. It Will Help The Ea To Assess The Needs And Identification Of The Suitable It System & Potential Solutions For Further Development In Its It Sector Appointing Need Assessment Consultants. It Will Also Finance For Purchasing Of It Instruments (hardware & Software) For Ea Staff And Employees. Component-c Project Audit: The Purpose Of The Component Is The Selection Of External Financial Auditor Who Would Perform Financial And Physical Audit Of The Project. Component-d Support To Pmu& Administrative Service Startup Workshop And Familiarization Visit: This Component Includes The Pmu’s Support Activities In The Form Of Office Equipment, Purchase Of Vehicles, Communication & Visibility, Training, Sensitization Awareness, Familiarization Visit, And Startup Workshop Etc. It Includes The Selection Of Individual Consultants (financial Management Specialist, Procurement Specialist And Monitoring And Evaluation Expert) For The Support To Pmu. Procurement Of Contracts Financed By The Islamic Development Bank (isdb) Will Be Conducted Through The Procedures As Specified In The Guidelines For The Procurement Of Goods, Works And Related Services Under Isdb Project Financing Including Procurement April 2019,(revised In February 2023) And Is Open To All Eligible Bidders As Defined In The Guidelines For The Procurement Of Consultant Services Under Isdb Project Financing Including Procurement April 2019 (revised In February 2023). Construction Of Houses With Related Facilities Under Component A Shall Strictly Follow The Requirements Stipulated In Paragraph 3.3 Procurement In Loans To Financial Intermediaries Of Isdb’s Relevant Procurement Guidelines. Procurement Of Goods Under Project’s Components B And D Will Be Undertaken Through Shopping And National Competitive Bidding Procurement Methods; Procurement Of Consultancy Services For Need Assessment Consultancy For It And The Consultancy For Development Of Convenient Housing Model Under Component B Will Be Conducted Through Quality And Cost-based Selection Method Among The Shortlist Of Domestic Firms; Procurement Of The Project Financial Auditing Services Under Component C Will Be Conducted Through Least-cost Selection Method Among The Shortlist Of Domestic Firms. Selection Of Financial Management Specialist, Procurement Specialist And Monitoring And Evaluation Expert Under Project’s Component D Will Be Undertaken Through Individual Consultant Selection Method Among The Domestic Consultants. Combination Of Direct Invitation With Local Advertisement For Procurement Of Goods Through Shopping Procurement Method. Specific Procurement Notices (spn) For Contracts To Be Bid Under The Islamic Development Bank’s Ncb Procedures For Goods, Quality And Cost Based Selection, Least Cost Selection And Individual Consultancy Services Procedures For Consultancy Services Will Be Announced, As They Become Available At The Web-site Of The Bangladesh Public Procurement Authority (bppa), Executing Agency (bhbfc) And In Local Newspapers. Interested Eligible Suppliers/firms/ Individuals Who Would Wish To Be Considered For The Provision Of Goods And Consulting Services For The Above-mentioned Project Or Those Requiring Additional Information, Should Contact The Beneficiary At The Address Below: Mohammad Nazrul Islam Deputy General Manager & Head Of Unit Foreign Financing And Project Unit For Rural And Peri-urban Housing Finance Project-second Phase Bangladesh House Building Finance Corporation 22 Purana Paltan (7th Floor), Tel: +88-02-47120610 Website: Www.bhbfc.gov.bd; E-mail: Bhbfc.project.pmu@gmail.com

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