MODIFICATION
A -- HYPERSONIC DEMONSTRATORS AND SYSTEMS ANALYSIS
- Notice Date
- 6/19/2002
- Notice Type
- Modification
- Contracting Office
- NASA/Langley Research Center, Mail Stop 144, Industry Assistance Office, Hampton, VA 23681-0001
- ZIP Code
- 23681-0001
- Solicitation Number
- SS0243
- Response Due
- 7/8/2002
- Archive Date
- 6/19/2003
- Point of Contact
- Robert J Rice, Contract Specialist, Phone (757) 864-2532, Fax (757) 864-8863, Email r.j.rice@larc.nasa.gov - Rosemary C. Froehlich, Contracting Officer, Phone (757) 864-2423, Fax (757) 864-8863, Email R.C.FROEHLICH@larc.nasa.gov
- E-Mail Address
-
Email your questions to Robert J Rice
(r.j.rice@larc.nasa.gov)
- Description
- The Sources Sought advertisement for the Hypersonic Demonstrators and Systems Analysis is hereby modified as follows: a. In order to correct a typographical error contained in the original announcement, sentence number 5, which begins, "Tasks may include but are not limited to:..." is hereby deleted from Part 1. Systems Analysis, Conceptual and Preliminary Design of Access-to-Space Vision Vehicles and Unpiloted Hypersonic Flight Vehicle Demonstrators and replaced with the following sentence: Tasks may include but are not limited to: definition of system architectures and vehicles that meet required missions; systems analysis of vehicles with new and advanced technologies for airframe and propulsion systems; definition of advanced ground operations and flight systems that lead to orders of magnitude improvement in cost and safety; vehicle system analysis and systems engineering and design; integration and performance assessment of low-speed and high-speed propulsion systems including turbine engines, rocket engines, ramjet and scramjet engines, and combined cycle engines (propulsion system design will not be in this task); aerodynamic and rothermodynamic analysis including computational fluid dynamics (CFD) analysis; inlet and nozzle flowpath; wind tunnel testing (unpowered and powered) of representative models (use of NASA and DoD wing tunnel facilities is anticipated); guidance, autonomous navigation and control definition and design; thermal protection; materials selection and airframe integration; vehicle system and subsystems design including vehicle purge, fuel system (hydrogen and hydrocarbon fuels are anticipated), structural, mechanical, thermal, power, avionics, and fuel systems; safety and hazards analyses; integrated performance analysis; vehicle reliability; crew safety; and preliminary maintenance, turn-around time and refurbishment concepts for recovered vehicles; and integration with potential launch and carrier vehicles, e.g., rockets or aircraft. b. The page limitation for capability statements is hereby changed from 7 pages to 10 pages (total). ALL OTHER INFORMATION CONTAINED IN THE ORIGINAL SOURCES SOUGHT ANNOUNCEMENT REMAINS UNCHANGED.
- Web Link
-
Click here for the latest information about this notice
(http://prod.nais.nasa.gov/cgi-bin/eps/bizops.cgi?gr=D&pin=23#101924)
- Record
- SN00096280-W 20020621/020619214019 (fbodaily.com)
- Source
-
FedBizOpps.gov Link to This Notice
(may not be valid after Archive Date)
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