Accession Number:

AD0509011

Title:

Performance of a Pyrolytic Graphite Reinformed Graphite felt Nozzle Insert Fired with a Fluorinated Propellant

Descriptive Note:

Technical rept.

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-01-01

Pagination or Media Count:

37.0

Abstract:

This report presents the results of testing performed on a nozzle insert which utilized pyrolytic graphite reinforced graphite felt as the throat material. The background for this testing, the design description, and the test conditions are also reported.

Subject Categories:

  • Rocket Engines
  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE