Hypersonics, Inc.

164 Ferne Court
Palo Alto, CA 94306
4 Employees

SBIR Award Summary

Total Number of Awards 11
Total Value of Awards $2.97MM
First Award Date 01/01/87
Most Recent Award Date 05/12/06

Key Personnel

Last Name Name Awards Contact
Conti Dr. Raul J. Conti 7 Message
Conti Paul J Conti 2

11 Awards Won

Phase 2 SBIR

Agency: Air Force
Topic: AF05-241
Budget: 05/12/06 - 03/15/09

The proposed innovation consists of developing and testing an integrated computational tool capable of predicting simultaneously the hypersonic flow over a reentry vehicle and the response of its thermal protection system, including surface ablation, recession, and in- depth thermal conduction, as well as internal pyrolysis in the case of charri...

Phase 1 SBIR

Agency: Air Force
Topic: AF05-241
Budget: 04/13/05 - 04/13/06

The proposed innovation consists of developing a stand-alone computational tool to predict simultaneously the hypersonic flowfield and the thermal response of the heatshield of vehicles entering the atmosphere at high speed, including the full coupling of the fluid an solid phenomena involved. In the past, the fluid and solid media have been an...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 95-1
Budget: 01/01/95 - 12/31/95
PI: Unavailable

Phase 1 SBIR

Agency: Air Force
Topic: AF93-105
Budget: 07/01/93 - 12/31/93

Phase 1 SBIR

Agency: Air Force
Topic: AF93-105
Budget: 07/01/93 - 12/31/93

Phase 2 SBIR

Agency: National Aeronautics and Space Administration
Topic: 92-2
Budget: 01/01/92 - 12/31/92
PI: Unavailable

THIS PROJECT EXPLORES THE BENEFITS OF A NEW COMPUTATIONAL MODEL FOR REACTING FLOWS. IT APPLIES TO NON-EQUILIBRIUM FLOWS, IN GENERAL, BUT IS SPECIALLY DESIGNED TO ADDRESS THE FREQUENT CONDITION IN HYPERSONIC FLOWS WHERE SOME OF THE REACTANTS ARE NEAR THERMOCHEMICAL EQUILIBRIUM, WHILE THE REMAINDER ARE OUT OF LOCAL EQUILIBRIUM. NONEQUILIBRIUM FLOW...

Phase 2 SBIR

Agency: Air Force
Topic: AF90-180
Budget: 09/12/91 - 08/31/93

A computer based algorithm is proposed that integrates an advanced Navier-Stokes hypersonic flow solver with material-response and shape-change technologies to create a powerful tool for ballistic or maneuvering reentry vehicle design.

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 91-1
Budget: 01/01/91 - 12/31/91
PI: Unavailable

Phase 1 SBIR

Agency: Air Force
Topic: AF90-180
Budget: 01/01/90 - 12/31/90

Phase 2 SBIR

Agency: Air Force
Topic: AF87-240
Budget: 05/10/89 - 04/30/91

CURRENT ANALYTICAL TOOLS USED IN THE DESIGN OF ANTENNA WINDOWS FOR REENTRY VEHICLES ARE LIMITED TO TWO SPACIAL DIMENSIONS, IN THE STREAMWISE AND IN-DEPTH DIRECTIONS, AND THEREFORE ARE UNABLE TO MODEL CORRECTLY THE EDGE EFFECTS THAT HAVE BEEN OBSERVED IN GROUND AND FLIGHT TESTS. THIS PROPOSAL ADDRESSES THE ADAPTATION OF ADVANCED COMPUTATIONAL FL...

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