PERFORMANCE CHARACTERISTICS OF COMPOUND A/HYDRAZINE PROPELLANT COMBINATION. VOLUME 2--TASK V APPENDIX.

Abstract

This volume of the final report is a tabular print and summary compilation of pertinent performance parameters for the ClF5/N2H4 propellant combination. In addition to an introductory section describing its use, performance in terms of standard rocket parameters are presented for chamber pressures of 1000, 700, 500, 300, and 100 psia at mixture ratios of 4.0, 3.5, 3.0, 2.8, 2.6, 2.4, 2.2, and 2.0. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1965
Accession Number
AD0380302

Entities

Organizations

  • Rocketdyne

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aliphatic Compounds
  • Chemical Compounds
  • Energetic Materials
  • Hydrazines
  • Propellants
  • Standards

Readers

  • Library and Information Science
  • Rocket Propulsion.