SHORT NOSE CONE STRUCTURE ASSEMBLY (X-1021425): AXIAL LOAD AND ELEVATED TEMPERATURE TESTS,
Abstract
A test was performed to determine the ability of an X-1021425 short nose cone to withstand an axial compressive load at elevated temperatures. The specimen withstood a 4275-lb axial compressive load for 60 sec. while the temperature was being increased from ambient to 870 F.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1958
- Accession Number
- AD0801764
Entities
People
- H. E. Brown
- W. L. Mclean
Organizations
- Lockheed Martin Missiles and Space