IN ORDER TO ACHIEVE INCREASED EFFICIENCY, LIFE, AND PERFORMANCE, ROCKET ENGINES REQUIRE OPERATION AT HIGHER AND HIGHER TEMPERATURES.

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$49,427.00
Award Year:
1983
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Award Id:
260
Agency Tracking Number:
260
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
12173 Montague Street, Pacoima, CA, 91331
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
() -
Business Contact:
Richard Kaplan
(213) 899-0236
Research Institute:
n/a
Abstract
IN ORDER TO ACHIEVE INCREASED EFFICIENCY, LIFE, AND PERFORMANCE, ROCKET ENGINES REQUIRE OPERATION AT HIGHER AND HIGHER TEMPERATURES. IN ORDER TO OBTAIN SUFFICIENT STRENGTH AT THESE TEMPERATURES, THE REFRACTORY METALS SUCH AS MOLYBDENUN, TUNGSTEN, TANTALUM, NIOBIUM, AND RHENIUM MUSTBE USED TO FABRICATE THE PARTS WHICH WILL BE EXPOSED TO THESE TEMPERATURES. THESE METALS AND THEIR STRUCTURALLY IMPORTANT ALLOYS HAVE NOTORIOUSLY POOR RESISTANCE TO OXIDATION IN THE TEMPERATURE RANGE WHERE THEIR STRENGTH CHARACTERISTICS ARE VITALLY NEEDED. PROTECTION, IN THE FORM OF COATINGS, FROM THE OXIDIZING ENVIRONMENT IS CRUCIAL FOR SUCCESSFUL OPERATION. CURRENT COATING TECHNOLOGY IS NOT SUFFICIENT TO ACHIEVE SATISFACTORY OPERATION. NEW OXIDATION RESISTANT COATING MATERIALS AND PROCESSES MUST BE DEVELOPED WHICH WILL PERMIT OPERATION IN THE 500 DEGREE C TO2000 DEGREE C TEMPERATURE RANGE. THE PLATINUM GROUP METALS OFFER A HIGH PROBABILITY OF SUCCESS AS OXIDATION RESISTANT COATING MATERIALS. ULTRAMET PROPOSES TO DEVELOP THE TECHNOLOGY REQUIRED TO CHEMICALLY VAPOR DEPOSIT DENSE, ADHERENT COATINGS OF IRIDIUM AND TO DETERMINE ITS OXIDATION PROTECTIVE TEMPERATURE RANGE. PHASE II WILL EXPAND THE EFFORT TO CVD THE OTHER PLATINUM GROUP METALS.

* information listed above is at the time of submission.

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