SATELLITE RENDEZVOUS TRAJECTORIES.
Abstract
Two types of satellite rendezvous trajectories were discussed: direct ascent from burnout and transfer from a parking orbit coplanar with the target orbit. Equations for the orbital elements and velocity requirements of the trajectories were presented, and numerical solutions were obtained for selected trajectories. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1962
- Accession Number
- AD0607849
Entities
People
- David A. Pierce