Propellant Residuals and Mixture Ratio for an F-2 Mission,

Abstract

This study was made to determine the propellant residuals and mixture ratio deviation of the engines on Centaur F-2 if the mixture ratio control system operated at its upper or lower failure mode limits or at null throughout the flight. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 28, 1962
Accession Number
AD0861787

Entities

People

  • E. Berlin
  • J. Luster
  • T. Shimizu

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Control Systems
  • Energetic Materials
  • Engineering
  • Failure Mode And Effect Analysis
  • Propellants
  • Residuals

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Regression Analysis.
  • Rocket Propulsion.