AERODYNAMIC LOAD TEST OF THE 7-31-21 PROTOTYPE LIGHT WEIGHT THRUST STRUCTURE, WS107A,
Abstract
The object of the test is to substantiate the structural integrity of a complete modified thrust structure under the influence of ultimate thrust and aerodynamic loads. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 09, 1959
- Accession Number
- AD0833380
Entities
People
- S. R. Harrison
Organizations
- General Dynamics