Optimum Program for Single Stage Rockets in Which Expellant is not the Source of Power

Abstract

The gravitational force and the thrust force are considered in the derivation of an optimum mass rate and exhaust velocity program.

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Document Details

Document Type
Technical Report
Publication Date
Oct 07, 1956
Accession Number
AD0606091

Entities

People

  • J. H. Irving

Organizations

  • TRW Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Energetic Materials
  • Materials
  • Motion
  • Propellants
  • Terminals

Fields of Study

  • Physics