SBIR/STTR Research Award

Increased Thrust to weight ratio for small Rocket Motors (Directed Attitude Control System)

Award identifier 00ce29dc8c3f919b28299169a3213b0c1b32e2dec8ff4c84c241b8a66686c984Awarding agency Department of Defense · Missile Defense Agency

Award amount

$69,691

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Missile Defense Agency
Recipient company
ROTORDYNAMICS-SEAL RESEARCH
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

An advanced engine modeling and simulation software package is proposed for optimization of small rocket motors. The analysis package is a completely integrated transient simulaton for all engine components, the overall engine performance, and theengine-vehicle performance. Higher thrust-to-weight engines for small rocket motors.

Technology keywords

Not reported

Agency intelligence

Department of Defense

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