Accession Number:

AD0274351

Title:

TITAN II. DYNA SOAR

Descriptive Note:

Corporate Author:

MARTIN CO BALTIMORE MD

Personal Author(s):

Report Date:

1962-03-15

Pagination or Media Count:

68.0

Abstract:

The use of storable, high energy and hypergolic pr pellants, Unsymmetrical Dimethyl Hydrazine UDMHHydrazine and Nitrogen Tetroxide N2O4, in Titan II and Titan III is an advancement in weapon and space systems. However, the intermixing reaction and toxicological properties of these propellants introduced a problem in the design of the destruct system for the booster. Tests were conducted to develop and verify a booster destruct system for use with these propellants.

Subject Categories:

  • Manned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE