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|VEP - |
Credit: ESA. 13,295 bytes. 225 x 186 pixels.
Other Designations: Vehicle Evaluation Payload. Class: Technology. Nation: Japan. Agency: Japan(Myojo).
Monitored H-2 launch vehicle performance. National name MYOJO. Provided a ranging function as well as functions to measure the acceleration and deformation, in order to confirm the accuracy of the H-2 rocket orbit injection and understand the environment of the payload equipment. Launching organization NASDA.
Total Mass: 2,391 kg.
03 February 1994
VEP Launch Site: Tanegashima . Launch Vehicle: H-2. Mass: 2,391 kg. Perigee: 449 km. Apogee: 36,261 km. Inclination: 28.6 deg.
Vehicle Evaluation Payload; monitored H-2 performance. Vehicle Evaluation Payload (VEP) MYOJO. Provides a ranging function as well as functions to measure the acceleration and deformation, in order to confirm the accuracy of the H-II rocket orbit injection and understand the environment of the payload equipme nt. Launch vehicle H-II rocket test flight H-II 1F. Launching organization NASDA. Launch time 2220:00 UT.
- 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
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Last update 12 March 2001.
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