SBIR/STTR Research Award
Constant Pressure Aerospike for Interceptor Axial Propulsion
Award amount
$99,982Program and phase
SBIR · Phase IAward year
2010Award details
- Awarding agency
- Department of Defense
- Branch
- Missile Defense Agency
- Recipient company
- Analytical Services, Inc.
- Proposal award date
- 2010-05-03
- Contract end date
- 2010-11-02
- UEI
- K5Y3MDHD2MB5
- Solicitation number
- 2009.3
- Topic code
- MDA09-001
Research abstract
Our proposed effort will be used to determine the feasibility of a deeply-throttleable aerospike engine that maintains constant specific impulse performance, regardless of the throttle setting. The design incorporates technology previously demonstrated under another SBIR, but extends it through incorporation of an aerospike nozzle.
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.
- Improved Stability of Double Base Propellants
- Low-Cost Manufacturing Technique for Advanced Regenerative Cooling for In-Space Cryogenic Engines
- Miniature Extendable Nozzles or Actuating Nozzles for Improved ISP of Divert and Attitude Control System (DACS) Thrusters
- Solid Rocket Motor for Ultralow Temperature Operation During the Mars Sample Return Mission
- Low-Cost Manufacturing Technique for Advanced Regenerative Cooling for In-Space Cryogenic Engines
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Modular Aerospike Engine
- Light Weight Controllable Thrust Actuation for Innovative Propulsion System for Missile Defense Interceptors
- Innovative Propulsion Systems for Missile Defense Interceptors
- Innovative Motor Propellant Technology
Contractor profile
Historical federal award activity, when published, is on that contractor profile. Matched by UEI only.