Accession Number:

AD0606091

Title:

OPTIMUM PROGRAM FOR SINGLE STAGE ROCKETS IN WHICH EXPELLANT IS NOT THE SOURCE OF POWER,

Descriptive Note:

Corporate Author:

THOMPSON RAMO WOOLDRIDGE INC LOS ANGELES CALIF

Personal Author(s):

Report Date:

1956-10-07

Pagination or Media Count:

17.0

Abstract:

The gravitational force and the thrust force are considered in the derivation of an optimum mass rate and exhaust velocity program.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE