Japanese geostationary communications satellite. One launch, 2002.09.10. DRTS (Data Relay Transponder Satellite) relayed images and data procured by the ADEOS 2 and ALOS satellites, and the KIBO module on ISS.
Nearly cubical (2.2 m x 2.4 m x 2.2 m) 2.8-ton (with fuel), 2.1-kW (from a 17 square-meter array) spacecraft with S- and Ka-band transponders, parked over 90° E.
DRTS/Kodama was built by Mitsubishi for the Japanese NASDA space agency and has a mass of 1300 kg (dry), plus a further 1500 kg of propellant at launch for its propulsion system. The apogee engine was a 500N downrated version of the 1700N LAPS-derived engine used in the earlier COMETS satellite. DRTS had a 3.6-meter Ka-band dish.
More... - Chronology...
First Launch: 2002.09.10.
Number: 1 .
Associated Launch Vehicles
H-2 Heavy lift Japanese indigenous launch vehicle. The original H-2 version was cancelled due to high costs and poor reliability and replaced by the substantially redesigned H-2A. More...
H-IIA 2024 Japanese orbital launch vehicle. Three stage vehicle consisting of 4 x Castor 4XL + 2 x H-II SRB-A boosters + two-stage core vehicle. More...
McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
NASA/GSFC Orbital Information Group Website, Web Address when accessed: here.
Space-Launcher.com, Orbital Report News Agency. Web Address when accessed: here.
Associated Launch Sites
Tanegashima Japan's main launch site for he larger N and H launch vehicles. In use for sounding rockets from 1967 and orbital launches from 1975. As of 2007 over 140 major launches had been made from the site. More...
2002 September 10 -
08:20 GMT - .
. Launch Complex
: Tanegashima Y
. LV Family
. Launch Vehicle
: H-IIA 2024
. LV Configuration
: H-2A/2024 s/n F3.
- DRTS - .
Payload: Kodama (DRTS-W). Mass: 2,800 kg (6,100 lb). Nation: Japan. Agency: NASDA. Manufacturer: Mitsubishi. Class: Communications. Type: Civilian communications satellite. Spacecraft: DRTS. USAF Sat Cat: 27516 . COSPAR: 2002-042B. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Launch delayed from August 2002. First operational flight of H-2A booster. DRTS (Data Relay Transponder Satellite) was a Japanese geostationary communications spacecraft which was to relay images and data procured by the to-be-launched ADEOS 2 and ALOS satellites, and the KIBO module on ISS, after being parked over 90° E. However the engine failed after a couple of burns. As of 2007 Mar 11 located at 90.76E drifting at 0.005W degrees per day.
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