Accession Number:

AD0395501

Title:

Advancement of Injector and Thrust Chamber Technology with ClF3 and MHF-3 Propellants.

Descriptive Note:

Technical rept. 21 Jan 66-1 Mar 67,

Corporate Author:

TRW SYSTEMS REDONDO BEACH CALIF

Personal Author(s):

Report Date:

1967-03-01

Pagination or Media Count:

206.0

Abstract:

This report covers an analytical and experimental program to generally advance the state of the art of rocket engine components applicable to prepackaged tactical weapon systems. The principal objective of the program was a thorough investigation of the feasibility of the TRW single-element coaxial injector concept with halogenated oxidizer systems. Specific tasks consisted of development and demonstration of a durable, stable, high performing injector with ClF3MHF-3 thrust chamber wall environmental studies thrust chamber materials evaluations ClF3Alumazine performance evaluations and boostsustain duty cycle demonstrations. Author

Subject Categories:

  • Combustion and Ignition
  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE