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HIGH TEMPERATURE RAKE PROBE FOR ARC-JET TESTS

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: N/A
Agency Tracking Number: 12269
Amount: $493,928.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1992
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
PO Box 5487
San Bernardino, CA 92412
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Henry L Moody
 (714) 889-2562
Business Contact
Phone: () -
Research Institution
N/A
Abstract

THE OBJECTIVE OF THE PROGRAM IS TO DESIGN RAKE PROBES THAT CAN ACCURATELY MEASURE AND MAP ARC-JET EXIST PLANE FLOW QUANTITIES. THREE RAKE PROBES SHALL BE DESIGNED THAT CAN MAP OUT THE AERODYNAMIC PROPERTIES OF THE TEST SECTION IN HIGH-ENTHALPY/HIGHPRESSURE ARC-JETS. THE FIRST PROBE SHALL BE A CYLINDRICAL PRESSURE/CALORIMETER RAKE THAT CAN BE SWEPT ACROSS THE TEST SECTION TO MEASURE PRESSURE, CONVECTIVE HEATING AND INFER ENTHALPY. THIS PROBE SHALL BE FABRICATED IN PHASE I. THE SECOND PROBE IS A RAKE WITH AXI-SYMMETIRIC PROBES TO CHARACTERIZE THE THREE-DIMENSIONAL FLOW BEHAVIOR OF THE TEST SECTION. THE THIRD PROBE SHALL BE USED TO INFER ENTHALPY.

* Information listed above is at the time of submission. *

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