ADVANCED THERMAL PROTECTION MATERIALS

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$50,000.00
Award Year:
1988
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Award Id:
6676
Agency Tracking Number:
6676
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
12173 Montague St, Pacoima, CA, 91331
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
RICHARD B KAPLAN
() -
Business Contact:
() -
Research Institute:
n/a
Abstract
COMPONENTS FOR AEROPROPULSION SYSTEMS WILL REQUIRE STRUCTURAL, MINIMUM-WEIGHT, REUSABLE THERMAL PROTECTION MATERIALS. THE LIMITATIONS OF CURRENTLY AVAILABLE MATERIALSARE TEMPERATURE, THERMAL SHOCK RESISTANCE, AND FRACTURE TOUGHNESS. BY AN INNOVATIVE APPLICATION OF CHEMICAL VAPOR DEPOSITION, ULTRAMET PROPOSES TO DEMONSTRATE THE FEASIBILITYOF FABRICATING COMPOSITE MATERIALS WHOSE ULTIMATE CAPABILITIES ARE: 1. 2200 DEGREE(") OR HIGHER OPERATING TEMPERATURES 2. OXIDATION RESISTANCE 3. INTRINSIC THERMAL CONDUCTIVITY LESS THAN 0.2 W/M.K 4. AREAL DENSITY LESS THAN 2.0 G/CM3 5. FLEXURAL STRENGTH AT ROOM TEMPERATURE OF 30,000 PSI AND AT 2200 DEGREE(C) OF 3000 PSI 6. METAL-LIKE FRACTURE TOUGHNESS AND THERMAL SHOCK RESISTANCE

* information listed above is at the time of submission.

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