LINEAR PROPORTIONAL CONTROL HOT GAS VALVE FOR SECONDARY INJECTION,

Abstract

Two linear proportional control hot gas valves were tested as an integral component of a liquid rocket chamber bleed system. One valve relied entirely on the refractory metal, tantalumtungsten alloy (Ta-10W), whereas the second valve used an arrangement of internal heat sinks, ceramic insulators and ablative plastic inserts to serve as thermal protection for the tungsten surfaces of the critical components. The refractory metal valve failed after three seconds of operation due to severe degradation of the Ta-10W alloy components. In contrast, the composite materials valve successfully completed four 12 sec duration tests, representing 48 sec of accumulative throttling operation without any parts replacement. The valve demonstrated excellent structural durability and reproducible control capability during cyclic throttling. It is firmly believed this design is capable of at least 20 sec of continuous throttling operation under the design mass flows of 5140 F combustion gases. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1964
Accession Number
AD0433751

Entities

People

  • F. P. Crommie
  • W. F. Lehman

Organizations

  • Picatinny Arsenal

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Bleed Systems
  • Composite Materials
  • Dielectrics
  • Gases
  • Heat Energy
  • Heat Sinks
  • Hot Gases
  • Joule Thomson Effect
  • Mass Flow
  • Materials
  • Metals
  • Refractory Metals
  • Secondary Injection
  • Tungsten

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Mathematics or Statistics
  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • Microelectronics