This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Other Designations: Integrated Rendezvous Target. Class: Technology. Nation: USA. Agency: NASA. Deployed from STS 41B 2/5/84.
SpecificationTotal Mass: 91 kg.
IRT Chronology
03 February 1984
IRT Launch Site: Cape Canaveral . Launch Vehicle: Shuttle. Mass: 91 kg. Perigee: 279 km. Apogee: 288 km. Inclination: 28.5 deg. Deployed from STS 41B 2/5/84; Integrated Rendezvous Target. Spent boosters, spent maneuvering stages, shrouds and other non-functional objects (US Cat D).
Bibliography:- 2 - McDowell, Jonathan, The United Nations Registry of Space Objects, Harvard University, 1997. HTML when accessed: http://hea-www.harvard.edu/QEDT/jcm/space/un/un.html
- 6 - JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. HTML when accessed: http://msl.jpl.nasa.gov/home.html
- 279 - McDowell, Jonathan, Launch Log, October 1998. HTML when accessed: http://hea-www.harvard.edu/~jcm/space/log/launch.html
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .