HIGH TEMPERATURE TEST ON THE MOD III GUIDANCE ANTENNA FOR THE MERCURY VEHICLE,
Abstract
An analysis of the Mercury vehicle guidance antenna indicates that it will experience considerable aerodynamic heating. The purpose of this report is to describe the test performed to determine to what extent the antenna performance will be affected when subjected to the temperatures anticipated. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 02, 1959
- Accession Number
- AD0833976
Entities
People
- V. J. Moffatt
Organizations
- General Dynamics