THE RELATIVE IMPORTANCE OF DENSITY, SPECIFIC IMPULSE AND OTHER SOLID PROPELLANT PROPERTIES IN THE FRAME OF LONG-TERM RESEARCH GOALS

Abstract

An analysis is made of the major goals in solid rocket propulsion development. These include high-specific impulse propellants and high propellant loading fraction.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1962
Accession Number
AD0283940

Entities

People

  • William E. Gordon

Organizations

  • Institute for Defense Analyses

Tags

DTIC Thesaurus Topics

  • Burning Rate
  • Chambers
  • Combustion
  • Combustion Chambers
  • Engines
  • Equations
  • Exhaust Gases
  • Low Density
  • Materials
  • Payload
  • Propellants
  • Rocket Engines
  • Rocket Propulsion
  • Safety Factor
  • Sea Level
  • Solid Propellants
  • Specific Impulse

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Rocket Propulsion.
  • Theoretical Analysis.