Heat-Exchanger for High Specific Impulse Maneuvering

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: N/A
Agency Tracking Number: 18071
Amount: $49,520.00
Phase: Phase I
Program: SBIR
Awards Year: 1992
Solitcitation Year: N/A
Solitcitation Topic Code: N/A
Solitcitation Number: N/A
Small Business Information
Combustion Sciences, Inc.
501 S. Sixth Street, Champaign, IL, 61820
Duns: N/A
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 John W. Black
 (217) 356-4497
Business Contact
Phone: () -
Research Institution
N/A
Abstract
Strategic defense missions place a premium on the performance capabilities of onboard propulsion systems. An innovative technique for producing very high impulse at excellent thrust-to-weight ratios is known as laser-powered heat-exchanger propulsion. A remotely stationed high power laser is used to heat a propellent gas within a rocket engine, and the heated gas is exhausted to generate thrust at very high specific impulses. Until now, laser propulsion research has focussed on the use of high-temperature plasmas to convert laser energy into propellant heat. CSI's approach will use a direct-absorption "heat exchanger" as the conversion mechanism, a technique which is far less complex yet offers specific impulse performance in the range of 500-1000 seconds. Such a propulsion system can increase the payload capacity of on-orbit orbital transfer vehicles, or can enhance the range capability of ground-based interceptors.

* information listed above is at the time of submission.

Agency Micro-sites

US Flag An Official Website of the United States Government