PROPELLANT PERFORMANCE AND GAS COMPOSITION. HANDBOOK, SUPPLEMENT II,

Abstract

Tables of rocket propellant performance are presented, including sea level impulses and vacuum specific impulses with corresponding pressures for integral values of area ratio up to 50. The concentration of the combustion products at area ratios that were nearest 10 and 40 are given. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 12, 1963
Accession Number
AD0425546

Entities

People

  • E. A. Cook
  • L. Schieler
  • S. A. Johnston

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustion
  • Combustion Products
  • Explosive Testing
  • Handbooks
  • Integrals
  • Propellants
  • Rocket Propellants
  • Sea Level
  • Specific Impulse

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Combustion and Flow Dynamics.
  • Library and Information Science