AIRCRAFT INTERFEROMETER DEVELOPMENT.
Abstract
In this report the special features of the three interferometers flown successfully in a KC-135 aircraft are discussed. The vibration disturbance in the aircraft required that the interferometer servo be made 'stiffer'. The steps taken to accomplish this are presented. The special shaker table used to check the interferometer for its vibration sensitivity is described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1969
- Accession Number
- AD0692518
Entities
People
- Alvan H. Bullard