Design and Development of Large Model Dual Component Exhaust Propulsion Systems,

Abstract

As far as super charging improvements carried out on large model dual component propulsion systems are concerned, they make the new systems completely different from the pressure regulated systems at the present time. From considerations of the three areas of thrust chamber design, performance, and system structure, operating conditions associated with new designs all have important technological advances. Test measurements have been carried out with regard to system levels through thrust chamber thermal tests. In conjunction with this, verifications have been carried forward in respect to propulsion system exhaust design life limits.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1996
Accession Number
ADA310488

Entities

People

  • Dong Wang
  • Ruiting Yang

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Chambers
  • Combustion
  • Combustion Chambers
  • Control Systems
  • Cycles
  • Engines
  • Film Cooling
  • Films
  • Ignition
  • Propulsion System Components
  • Propulsion Systems
  • Spacecraft
  • Specific Impulse
  • Storage Tanks
  • Thermodynamic Processes
  • Thin Films
  • Thrust Chambers

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Systems Analysis and Design