Low Cost Free-Flight Scramjet Test Technique

Award Information
Agency:
Department of Defense
Branch
Defense Advanced Research Projects Agency
Amount:
$98,748.00
Award Year:
1998
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Award Id:
40428
Agency Tracking Number:
40428
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
77 Raynor Ave, Ronkonkoma, NY, 11779
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Robert Bakos
(516) 737-6100
Business Contact:
() -
Research Institute:
n/a
Abstract
Development of a low-cost, near term approach to flight testing a hypersonic, storable fuel, scramjet engine using ballistic range technology is proposed. Flight-testing is easily the most expensive component of the triad of computational fluid dynamics (CFD), ground-testing and flight-testing needed to develop and demonstrate sustained and accelerating airbreathing flight at hypersonic speeds. Cost reduction by a factor of 100 to 200 relative to rocket launching a full-scale engine is sought. The proposed approach will leverage off GASL's low-cost, rapid prototyping capabilities for scramjet engines for wind tunnels and for NASA's Hyper-X flight test program, Boeing's prior experience in launching a scramjet from the SHARP gun at LLNL, and prior Army Research Lab personnel in data telemetry from gun-launched munitions. Essential aspects of the proposed approach are use of closely coordinated CFD and ground-testing to maximize the flight data yield and minimize the risk and cost, and use of a controlled flight environment to permit proper simulation of flight dynamic pressure. Flight speeds from Mach 6 to 12 are considered within existing ballistic range capabilities. Mach 8 is the proposed test point since it supports the goals of the HyTech and ARRMD programs.

* information listed above is at the time of submission.

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