Accession Number:

AD0293892

Title:

AN EXPLICIT SOLUTION TO THE POWERED FLIGHT DYNAMICS OF A ROCKET VEHICLE

Descriptive Note:

Corporate Author:

AIR FORCE SYSTEMS COMMAND SPACE SYSTEMSDIV LOS ANGELES CA

Personal Author(s):

Report Date:

1962-10-31

Pagination or Media Count:

55.0

Abstract:

A general explicit solution to the powered flight dynamics of a rocket vehicle having constant thrust and constant effective exhaust velocity is presented. The use of this solution in guidance techniques is demonstrated.

Subject Categories:

  • Surface-Launched Guided Missiles
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE