PACKAGEABLE HIGH EXPANSION-RATIO NOZZLES FOR SOLID-PROPELLANT ROCKET MOTORS. VOLUME II.

Abstract

The purpose of this program is to develop and demonstrate practical, usable, packageable exit cones which can be stored for extended periods, be deployed reliably, and be easily scaled for direct application to future high-performance solid rocket systems which include thrust vector control.

Document Details

Document Type
Technical Report
Publication Date
Aug 31, 1967
Accession Number
AD0820625

Entities

People

  • William K Peters

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Cooperation
  • Energetic Materials
  • Materials
  • Propellants
  • Rocket Engines
  • Rockets
  • Solid Propellants

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Rocket Propulsion.