You are here
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
Name: Henry L Moody
Phone: (714) 889-2562
Phone: (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. *