What is it about?
Interplanetary missions can maximize scientific return by sending both an orbiter and a lander or probe to their destination. We develop a method that uses atmospheric flight to co-deliver both types of spacecraft from a single approach trajectory.
Featured Image
Read the Original
This page is a summary of: Flight Mechanics Feasibility Assessment for Co-Delivery of Direct-Entry Probe and Aerocapture Orbiter, Journal of Spacecraft and Rockets, September 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34953.
You can read the full text:
Contributors
The following have contributed to this page
