Low Thrust Bipropellant Engine/Redundant Seat Valve Assembly.

reportActive / Technical Report | Accession Number: ADA150293 | Need Help?

Abstract:

The Air Force Rocket Propulsion Laboratory awarded a contract in 1982 to Rocketdyne to demonstrate the performance of two low-thrust bipropellant engineredundant seat value assemblies. The program focused on the integration and demonstration test of two independently developed redundant seat bipropellant valves and two low-thrust beryllium engines. The test program conducted on the redundant seat valveengine assemblies included laboratory checkouts, random launch vibration simulation, calibration hot-fire, and durability hot-fire. This report contains a description of the test hardware and documents the results of the completed test program. Originator-furnished keywords include Low thrust, Satellite thrusters, Beryllium thrusters, Rocket engines, Bipropellant, Redundant seat, Redundant coils, Torquemotor, Solenoid, N204MMH, Long life.

Author(s):
De Gaetano, E. A.
Author Organization(s):
ROCKWELL INTERNATIONAL CANOGA PARK CA ROCKETDYNE DIV
Descriptive Note:
Final rept. Sep 82-Aug 84,
Pagination:
0110

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
RI/RD84-196, AFRPL-TR-84-066
Contract/Grant Number(s):
F04611-82-C-0064
Task Number(s):
11
Project Number(s):
3058
Monitor Series:
TR-84-066
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Modernization Areas:
Space
Communities of Interest:
Space
Descriptor(s):
*VALVES, *ROCKET ENGINES, TEST AND EVALUATION, COILS, PERFORMANCE(ENGINEERING), ENDURANCE(GENERAL), LONG LIFE, BERYLLIUM, REDUNDANCY, THRUSTERS, TORQUE, SEATS, BIPROPELLANTS, SOLENOID VALVES
Field(s)/Group(s):
Pumps, Filters, Pipes, Tubing, Fittings and Valves, Liquid Propellant Rocket Engines
Keyword(s):
WUAFRPL305811LY, PE62302F
Report Date:
1984 Dec 01