INVESTIGATION OF SPRING RATE CHARACTERISTICS ON STUB TANK AND SUSTAINER THRUST CONE OF TSTS NO. 3,
Abstract
The objective of this test was to determine the deflection magnitude of the fuel tank and sustainer thrust cone, at various locations, for each of several loading conditions. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 30, 1959
- Accession Number
- AD0833175
Entities
People
- D. R. Haynes
Organizations
- General Dynamics