Accession Number:

AD0513619

Title:

Injector/Chamber Scaling Feasibility Program. Volume II. Ablative Chamber Design and Long Duration Testing

Descriptive Note:

Final rept. 11 Dec 1968-5 Feb 1970

Corporate Author:

TRW SYSTEMS GROUP REDONDO BEACH CA

Personal Author(s):

Report Date:

1970-07-01

Pagination or Media Count:

176.0

Abstract:

Three ablative thrust chambers were designed, fabricated and test fired. Low-cost liner materials were used in three chamber designs the material selection was based upon subscale test data. Low-cost fabrication techniques were employed throughout. Several fabrication problems with low-cost materials were delineated. Four ablative materials were evaluated in the test program.

Subject Categories:

  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE