Accession Number:

AD0766022

Title:

Solid Propellant Ballistic Missile,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1973-07-25

Pagination or Media Count:

714.0

Abstract:

In the report, on the basis of the materials published in the open Soviet and foreign presses, the tasks of ballistic design of solid-propellant rockets are formulated. Typical structural diagrams are given for guided ballistic missiles with engines on solid propellant and the methods of calculation of the elements of their trajectories in connection with the tasks of ballistic design. Approximation methods are illuminated and the concept given about the precise methods of ballistic design.

Subject Categories:

  • Guided Missiles
  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE