Gelled LH2/UFAL/LOX Propellant System

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$70,000.00
Award Year:
2001
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Agency Tracking Number:
NASA576
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Orbital Technologies Corporation
Space Center, 1212 Fourier Drive, Madison, WI, 53717
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Dr. Chiaverini
Project Manager
(608) 827-5000
chiaverinim@orbitec.com
Business Contact:
Dr. Eric E Rice
President/CEO
(608) 827-5000
ricee@orbitec.com
Research Institution:
n/a
Abstract
ORBITEC proposes to use ultra-fine aluminum powder (UFAL) to develop a gelled LH2 fuel and LOX propellant system. This innovation will increase the performance and density of LH2/LOX and the combustion efficiency of LH2/Al/LOX for use in rockets and combined-cycle vehicles. Lighter, higher-performing vehicles will result. Project objectives include development of a subscale rocket engine with which to test LH2/UFAL/LOX over a range of operating conditions, analysis and correlation of experimental data, and preliminary design of larger rocket and ramjet engines for Phase II. In Phase I, a prototype rocket will be test fired. In Phase II, a larger rocket engine will be developed and tested and a prototype ramjet engine will be tested to validate the performance of LH2/UFAL with air for combined-cycle vehicles. It is anticipated that the test results will show high specific impulse, high combustion efficiency, and improved propellant density. NASA applications include planetary propulsion, sounding rockets, various types of launch vehicles, space engines for near-Earth and interplanetary missions, and combined-cycle vehicle engines.

* information listed above is at the time of submission.

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