ORSC Methane Ascent/Descent Engine Technology Development
Award amount
$124,894Program and phase
SBIR · Phase IAward year
2015Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- SPECIAL AEROSPACE SERVICES
- Proposal award date
- 2015-06-17
- Contract end date
- 2015-12-17
- UEI
- QJMZBMHTMUE3
- Solicitation number
- Not reported
- Topic code
- H2.01
Research abstract
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Autonomous Launch Vehicle Interface System
- Autonomous Launch Vehicle Interface System
- Selective Emission of Light Utilizing Functionally-Graded Energetic Materials
- Anisotropic Property Manipulation of Selective Laser Melted GRCop-84
- Selective Emission of Light Utilizing Functionally-Graded Energetic Materials
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Cuberover for Lunar Resource Site Evaluation
- Additively Manufactured Monolithic LOx/Methane Vortex RCS Thruster
- Diamond_Copper Materials Based Solution for Improved Engine Performance
- Additive Manufacturing Technology for a 25,000 lbf LOX/Methane Mars Ascent Engine
- Ultrasonic Additive Manufacturing for High Performance Combustion Chambers
Research funding history
8 SBIR/STTR records share this UEI (2011–2021). Reported award amounts total $2,615,008. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense