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Generic aerocapture atmospheric entry study. volume 2: trajectory appendices
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1980 |
| Description | Aerothermodynamic and control system parameters and performance are discussed. Aerocapture trajectories were run for several combinations of entry path angles and velocities for the SO2P, MSR, and Uranus missions. The SO2P trajectories represent a Titan atmospheric entry for orbit about Saturn; the MSR trajectories represent a Mars atmospheric entry for orbit about Mars; similarly, the Uranus trajectories enter an Uranus atmosphere to achieve orbit about Uranus. |
| File Size | 2454087 |
| Page Count | 159 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810012570 |
| Archival Resource Key | ark:/13960/t0kt1h810 |
| Language | English |
| Publisher Date | 1980-10-24 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Interplanetary Trajectories Interorbital Trajectories Spacecraft Reentry Orbit Transfer Vehicles Thermal Protection Spacecraft Trajectories Orbital Velocity Atmospheric Entry Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
