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.
Descriptors:
- *ROCKET NOZZLES
- *NOZZLE INSERTS
- HEAT TRANSFER
- ALUMINUM COMPOUNDS
- CORROSION
- PASSIVE SYSTEMS
- COOLING
- NITRIDES
- EROSION
- COPPER
- FLUORINE
- LIQUID PROPELLANT ROCKET ENGINES
- TEMPERATURE CONTROL
- COOLANTS
- SILICON COMPOUNDS
- LIQUID ROCKET FUELS
- FAILURE(MECHANICS)
- FLUORIDES
- HEAT SINKS
- HALOCARBON PLASTICS
- LIQUEFIED GASES
- LIQUID ROCKET OXIDIZERS
- NOZZLE THROATS
- NOZZLE GAS FLOW
- METHYL HYDRAZINES
- PYROLYTIC GRAPHITE
- GASKETS
- CHLORINE COMPOUNDS
Subject Categories:
- Rocket Engines
- Liquid Propellant Rocket Engines