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Performance of recoverable single and multiple space tugs for missions beyond earth escape
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zimmerman, A. V. |
| Copyright Year | 1972 |
| Description | A recoverable space tug launched by the space shuttle to provide the required post-orbital propulsion needed for placement of unmanned satellites is described. The space tug will also be used to launch interplanetary spacecraft from low earth orbit. The performance of single and multiple space tugs (in tandem) for launching spacecraft beyond earth escape is summarized. Trajectories are developed that allow recovery of the tugs whenever practical. The effects of important tug and trajectory parameters on performance are presented. It is concluded that a single tug can inject spacecraft to Mars or Venus and still be recovered. The use of several tugs in tandem can provide a significant increase in capability over the use of a single tug. The more difficult missions involve a mix of recovered and expended tugs. |
| File Size | 1239085 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720026202 |
| Archival Resource Key | ark:/13960/t8dg1hf1f |
| Language | English |
| Publisher Date | 1972-01-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Spacecraft Performance Space Missions Low Earth Orbits Space Shuttles Space Tugs Mission Planning Spacecraft Recovery Spacecraft Propulsion Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |