This procurement is a result of a NASA research announcement (NRA), NNH06ZEA001N-SUP3 that was issued on may 23, 2006 to solicit proposals in support of NASA's aeronautics research mission directorate…
Ended Definitive Contract Awarded Last action
- Contract number
- NND08AA99C
- Awardee
-
Eagle Aeronautics, Inc. UEI SHWHBGTHK691
- Awarding agency
-
Armstrong Flight Research Center
National Aeronautics and Space Administration
- Obligated
- $306,039
Award facts
- Opportunity
- Contract value 100% obligated
- $306,039.36 Current and potential, with all options
- Completion date 100% complete
- Current and potential, with all options
- NAICS code
- 541712 Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
- Set-aside
- No set-aside
- Competition
- Full and Open Competition · 2 offers Negotiated Proposal / Quote
- Pricing
- Firm Fixed Price
- Place of performance
- Hampton, VA 23669, USA
Award details come from SAM.gov/FPDS.
Transactions
| Action | Obligated | Date |
|---|---|---|
| Close Out | -$0 | |
| Other Administrative Action | $0 | |
| Other Administrative Action | $0 | |
| Other Administrative Action | $0 | |
| Other Administrative Action | $0 | |
| Funding Only Action | $22,066 | |
| Funding Only Action | $74,467 | |
| Funding Only Action | $79,058 | |
| Original award | $130,448 |
Description
This procurement is a result of a NASA research announcement (NRA), NNH06ZEA001N-SUP3 that was issued on may 23, 2006 to solicit proposals in support of NASA's aeronautics research mission directorate (armd). One of the proposals, the measurement of free-stream mach number, pressure, temperature, density, and angle-of-attack at supersonic speeds using conical and wedge probes (proposal number 06-SUP3-06-0012) submitted by eagle aeronautics, INC., was selected to support the aviation safety program, and in particular the supersonic s project 3. The primary goal of this NRA to provide NASA with flight safety enhancement through a process to identify accurate measurement of mach number and angle of attack at transonic and supersonic speeds. This measurement is important for many reasons in carrying out flight research such as accurately defining the instantaneous in-flight conditions of the generating and probing aircraft along with its flow-field. IT is also important in avoiding focused booms by controlled ascent and descent to and from cruise of commercial supersonic aircraft. Changes in altitude and attitude and the resultant changes in free stream pressure and temperature along with changes in velocity all contribute to mach number variations. Eagle aeronautics, INC. Will work with NASA langley research center, NASA dryden flight research center and a qualified contractor will manage the design, fabrication and testing of two conical and two wedge probes for use in wind tunnels and also designed for use on full-scale supersonic aircraft. These probes would be designed for use in acquiring exacting near-field sonic boom signatures during wing tunnel tests and in-flight test along with the vehicle mach number, flow angularity and angle-of-attack not previously acquired with the current probe system that are subject to error due to systems lag and balloon measurements of required atmospheric properties. Comparisons of the results of the conical and wedge probes will be made with those in current use. This acquisition will result in a 15 month firm-fixed price contract to be conducted by eagle aeronautics, INC. Of hampton, VA for a total amount of $209,506.56.
Quick answers
Who was awarded contract NND08AA99C?
NND08AA99C was awarded to Eagle Aeronautics, Inc. by Armstrong Flight Research Center (National Aeronautics and Space Administration) on June 18, 2008.
How much is contract NND08AA99C worth?
The government has obligated $306,039 on NND08AA99C.
Was contract NND08AA99C competed?
The extent of competition for NND08AA99C was full and open competition. The government received 2 offers.
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