SBIR/STTR Research Award

Design of a Reaction Control Assisted Flight Control System for Small Airframes

Award identifier f7f2c6a25bb545cbfef24698737206d5fc682a5536730616ff4c9b861f7024e5Awarding agency Department of Defense · Air Force

Award amount

$94,718

Program and phase

SBIR · Phase I

Award year

1997

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ISX CORP.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

ISX proposes to design a novel low-volume hot gas propulsion system for missile translational maneuvers. A hybrid rocket motor hot gas generator, custom thruster diverter valve assembly specialized control system and an attendant guidance algorithm should null the missile body axis rotations during a translational maneuver. Simple vehicle planar (3 DoF) dynamics coupled with hardware element and control system models will be used to build a simulation to validate the designs.

Technology keywords

Not reported

Agency intelligence

Department of Defense

Back to SBIR/STTR Research Awards

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