Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume III--Part A - Screening and Optimization Analyses.

Abstract

Part A of this volume provides: the study ground rules and vehicle environments to which the propellant feed system is designed; a Configuration Optimization Study that allowed selection of the propellant tanks and shell; an impact study of an integrated attitude control system (F2/H2) as compared to the reference Compound A/MHF-5 attitude control system; and screening and optimization analyses that led to the design requirements for the external load-carrying shell, engine thrust structure, thermal control coating, engine actuators, tank support struts, insulation systems, ground hold vent-free oxidizer tank system and flight tank-pressure-control system.

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1970
Accession Number
AD0511038

Entities

Organizations

  • Rocketdyne

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Actuators
  • Attitude Control Systems
  • Control Systems
  • Cooperation
  • Environment
  • Insulation
  • Optimization
  • Propellant Tanks
  • Propellants
  • Propulsion Systems

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Robotics and Automation.
  • Rocket Propulsion.

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems