SOLICITATION NOTICE
A -- CREW LAUNCH VEHICLE WIND TUNNEL TEST IN POLYSONIC TEST FACILITY
- Notice Date
- 3/13/2007
- Notice Type
- Solicitation Notice
- NAICS
- 488190
— Other Support Activities for Air Transportation
- Contracting Office
- NASA/Langley Research Center, Mail Stop 144, Industry Assistance Office, Hampton, VA 23681-0001
- ZIP Code
- 23681-0001
- Solicitation Number
- NNL07192264Q
- Response Due
- 3/23/2007
- Archive Date
- 3/13/2008
- Small Business Set-Aside
- N/A
- Description
- NASA/LaRC has a requirement to conduct a wind tunnel test in a Polysonic Wind Tunnel (PSWT). The ARES I project is preparing an aerodynamic database that characterizes the vehicle throughout the speed regime of ascent flight where aerodynamic effects are important. This speed regime begins at liftoff and continues through first-stage separation or about Mach 6. The aerodynamic database will be used to determine the ARES I performance, stability & control effectiveness, and structural stability. NASA/LaRC intends to purchase the services from Boeing, Inc. who is the only known responsible source. To support the assessment of the ARES I configuration, the data to develop the aerodynamic database is required over the ascent Mach range. A 0.01-scale ( ~ 38? long) wind tunnel model has been built to test at NASA LaRC?s Unitary Plan Wind Tunnel (UPWT), for the Mach range 1.5 to 4.6. Data is required at the lower speeds for the initial phase of ascent. The Boeing Polysonic Wind Tunnel test covers the Mach range 0.4-1.6 providing data for the early ascent phase for ARES I flight. This facility allows the use of the newly fabricated model, sting, and balance hardware. There are no NASA facilities available with this Mach range and size. The Boeing Polysonic tunnel is the only known blow-down facility with the specific Mach number range, Reynolds number, and size to satisfy the wind tunnel testing requirement. Also, in support of the ARES I program, several configurations have already been tested and databases have been developed. The previous configurations were tested in the LaRC UPWT and the Boeing Polysonic Wind Tunnel to obtain the data to be used in developing the aerodynamic databases. In order to have tunnel to tunnel and database to database comparisons, similar facilities need to be utilized. This eliminates some of the uncertainty in the aerodynamic database, thus reducing risk to the program. The authority for this action is the test program for commercial items (section 4202 of the Clinger-Cohen Act of 1996), and 10 USC 2304(c)(1). The Government intends to acquire a commercial item using FAR Part 12 and Part 13.5, Test Program for Certain Commercial Items. Interested organizations may submit their capabilities and qualifications to perform the effort in writing to the identified point of contact not later than 4:30 p.m. local time on March 23, 2007. Such capabilities/qualifications will be evaluated solely for the purpose of determining whether or not to conduct this procurement on a competitive basis. A determination by the Government not to compete this proposed effort on a full and open competition basis, based upon responses to this notice, is solely within the discretion of the government. Oral communications are not acceptable in response to this notice. All responsible sources may submit an offer which shall be considered by the agency. An Ombudsman has been appointed. See NASA Specific Note "B". Any referenced notes may be viewed at the following URLs linked below.
- 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#123909)
- Record
- SN01250134-W 20070315/070313221553 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
| FSG Index | This Issue's Index | Today's FBO Daily Index Page |