Autonomous Navigation Technology Altimeter - Conceptual Design Study.
Abstract
Work was performed during a study program to define the parameters of a low duty cycle orbital space radar altimeter which could be used to update the autonomous navigation of earth satellites without betraying the satellite location. This report also contains the general constraints of space altimetry and a general guideline to the design of space altimeters.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 31, 1975
- Accession Number
- ADA008183
Entities
People
- Gary A. Murdock
- Walter Pagels
Organizations
- Teledyne Technologies