Accession Number:

AD0613962

Title:

TRANSIENT CHAMBER PRESSURE AND THRUST IN SOLID ROCKET MOTORS

Descriptive Note:

technical note

Corporate Author:

BROWN ENGINEERING CO INC HUNTSVILLE AL RESEARCH LABS

Personal Author(s):

Report Date:

1965-03-01

Pagination or Media Count:

37.0

Abstract:

An analysis of solid rocket motors was made in order to find the chamber pressure and thrust during the transient periods of buildup and decay. The results are differential equations and solutions of closed form.

Subject Categories:

  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE