NASA Dryden Flight Research Center, Mail Stop D-1044/XAA/LEB, P.O. Box 273, Edwards, CA 93523-0273

17 -- ROCKET MOTORS FOR USE IN HYPERSONICS OPERATIONS AND METHODOLOGY EXPERIMENT SOL RFO4-00030(LEB) DUE 052495 POC Contact Point: Louann E. Beu, Contracting Officer, (805) 258-3333, FAX (805) 258-2904 Rocket motors to be used in Hypersonics Operations and Methodology Experiment (HOME). The contractor shall design, fabricate and deliver to the designated test site area listed in the (SOW), three (3) rocket motor systems with the described specifications. Includes performing on instrumented static test of the rocket motor system including the measurement of thrust and booster pressure and post-test inspection of the motor. Post-test data reduction, includes the calculation of thrust, booster pressure, and specific impulse versus time. Provide detailed engineering drawings. Required delivery date on or before January 1, 1996. Approximate Specifications: Rocket Motor Weight-200 pounds; Burn Time: 5 seconds; Average Sea Level Thrust: 7500 pounds; Diameter: 7inches; Length: 100 inches. This procurement is being conducted under the NASA MidRange Pilot Test Program approved by the Office of Federal Procurement Policyon April 16, 1993. Request for copies of the RFO must be submitted in writing. Transmission by facsimile to (805) 258-2904 or by Internet E-mail to Louann_Beu@qmgate.dfrc.nasa.gov is acceptable. All responsible business sourcesmay submit an offer which shall be considered by the agency. (0122)

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