Accession Number:

AD0756850

Title:

Design Integration Test Requirements - Dyna-Soar

Descriptive Note:

Corporate Author:

BOEING CO SEATTLE WA

Personal Author(s):

Report Date:

1962-05-11

Pagination or Media Count:

94.0

Abstract:

The report contains the design integration test requirements for the Dyna-Soar Program and shall serve as the official source for Project Section and Staff usage. The document is designed to provide a single point of reference for all design integration test requirements and shall be used in generating the development test plans. Design integration tests consist of engineering testing wherein system design variables are investigated to verify the physical and functional capability and compatibility of mated subsystems using hardware completely representative of production configuration.

Subject Categories:

  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE