Minimum Cost Design (MCD) Material Screening. Test Report No. 1 - Haveg 41

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Abstract:

This is the first of a series of reports describing the results of test firings conducted to determine the performance of low-cost ablative materials which are candidates for use as thrust chamber and nozzle liners for MCD Minimum Cost Design Booster engines. This report describes the test of Haveg 41, an ablative composed of phenolic resin and asbestos fibers.

Author(s):
Hintz, James A.
Author Organization(s):
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
Descriptive Note:
Technical rept.
Pagination:
0026

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFRPL-TR-69-10
Project Number(s):
AF-305803KRD
Monitor Series:
AFRPL
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
*BOOSTER ROCKET ENGINES, ABLATION, ACCEPTABILITY, AGING(MATERIALS), ASBESTOS, BONDING, CAPTIVE TESTS, CATALYSIS, CATALYSTS, COMBUSTION CHAMBER LINERS, MOLDING MATERIALS, MOLDINGS, NOZZLE INSERTS, NOZZLE THROATS, PHENOLIC PLASTICS, ROCKET NOZZLES
Field(s)/Group(s):
Plastics, Combustion and Ignition, Rocket Engines
Keyword(s):
HAVEG 41 MATERIAL, HAVEG 41F MATERIAL, *NOZZLE LINERS, SEGMENTED LINERS
Report Date:
1969 Jan 01