Accession Number:

AD0851313

Title:

Critical Engine Components Minimum Temperature Study Missile 36D,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1960-05-20

Pagination or Media Count:

44.0

Abstract:

The report presents the results of a critical engine components minimum temperature study using Missile 36D.

Subject Categories:

  • Thermodynamics
  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE