Accession Number:

AD0395844

Title:

Development and Demonstration of Ablative Thrust Chamber Assemblies Using LF2/N2H4 Blend Propellants

Descriptive Note:

Rept. no. 2 (Final), 1 Sep 1966-19 Aug 1968

Corporate Author:

AEROJET-GENERAL CORP SACRAMENTO CA LIQUID ROCKET DIV

Report Date:

1969-01-01

Pagination or Media Count:

371.0

Abstract:

The exploratory development effort included the design, fabrication, and testing of injectors, ablative thrust chambers, and a radiation-cooled- divergent nozzle extension.

Subject Categories:

  • Laminates and Composite Materials
  • Combustion and Ignition
  • Liquid Propellant Rocket Engines
  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE