Further Developments in a Parametric Study of Ramrocket Performance

Abstract

The performance of a ramrocket is estimated for a set of reference conditions and then the effect on performance of variable altitude, radial injection of the primary jet, variable intake pressure recovery and different levels of secondary combustion efficiency are each examined in turn. The results are presented graphically in terms of specific impulse.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1985
Accession Number
ADA161906

Entities

People

  • Lincoln Erm

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Chemistry
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Computer Programs
  • Exhaust Nozzles
  • Flight Speeds
  • Flow
  • Gases
  • Mach Number
  • Mass Flow
  • Nozzles
  • Propellants
  • Ramjet Engines
  • Sea Level
  • Specific Impulse

Readers

  • Combustion and Flow Dynamics.