Accession Number:

AD0851135

Title:

A Preliminary Comparison of Missile Staging Methods,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

Report Date:

1954-11-17

Pagination or Media Count:

34.0

Abstract:

The purpose of the missile design and performance analysis was to obtain certain weight vs. range relationships for missiles of various staging methods. In the study missile size, takeoff thrust to weight ratio, and ratio of second stage thrust to first stage thrust are treated as variables. Author

Subject Categories:

  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE