SCALE ATLAS VERNIER ROCKET FLAME EXPANSION STUDIES,

Abstract

This report describes test procedures for determining the possibility of vernier motor exhaust impingement heating. A one-tenth scale model rocket and an altitude chamber were utilized.

Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1960
Accession Number
AD0842156

Entities

People

  • R. J. Sergeant

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Altitude Chambers
  • Chambers
  • Scale Models

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Rocket Propulsion.