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An autonomous rendezvous and docking system using cruise missile technology
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jones, ED Nicholson, Bruce |
| Copyright Year | 1991 |
| Description | In November 1990 General Dynamics demonstrated an AR&D system for members of the Strategic Avionics Technology Working Group. This simulation utilized prototype hardware derived from the Cruise Missile and Centaur avionics systems. The object of this proof of concept demonstration was to show that all the accuracy, reliability, and operational requirements established for a spacecraft to dock with Space Station Freedom could be met by the proposed AR&D system. |
| File Size | 204177 |
| Page Count | 2 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930012243 |
| Archival Resource Key | ark:/13960/t3wt3kq7x |
| Language | English |
| Publisher Date | 1991-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Centaur Launch Vehicle Autonomous Navigation Prototypes Orbital Rendezvous Space Station Freedom Spacecraft Docking Cruise Missiles Avionics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
