MAXIMUM PAYLOAD IN ORBIT.

Abstract

An existing multistage rocket booster is considered along with a variable payload stage. For a given launch weight, the fuel allocation to each stage and the thrust-direction program are determined which will place the maximum payload into a specified orbit. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1961
Accession Number
AD0637670

Entities

People

  • A. E. Bryson

Organizations

  • Lockheed Martin Missiles and Space

Tags

DTIC Thesaurus Topics

  • Booster Rocket Engines
  • Rockets

Readers

  • Control Systems Engineering.
  • Missile Defense Systems.

Technology Areas

  • Space
  • Space - Orbital Debris