Accession Number:

AD0861349

Title:

Multi-Stage Launch Vehicle Performance Exchange Ratios,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1962-03-06

Pagination or Media Count:

14.0

Abstract:

A series of equations has been developed relating the changes in final stage burnout weight, payload weight and expendable propellant weight to changes in jettison weight, expendable propellant weight and specific impulse of any stage of a multi-stage launch vehicle. Author

Subject Categories:

  • Liquid Rocket Propellants
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE