Mission Demonstration Satellite 1 (MDS-1) or Tsubasa (COSPAR 2002-003A, SATCAT 27367) was a Japanese technology test mission. It was launched by the second H-2A on February 4, 2002 from the Tanegashima Space Center. After the launch, MDS-1 was renamed Tsubasa, meaning wings in Japanese.[1] Tsubasa was placed in a geostationary transfer orbit (GTO). It ended its operational phase on 26 February 2003.[2] A similar mission, MDS-2, was cancelled.[3]
The purpose of the mission was to test the performance of commercial off-the-shelf components, including solar batteries, semiconductors and computers.[1][2] MDS-1 also carried instrumentation to observe how changes in the environment as the satellite passed through the Van Allen radiation belts affected the performance of each component. Among these instruments were a dosimeter using radiation-sensitive field effect transistors,[4] a magnetometer, and a device for tracking heavy ions.[5] During the mission, MDS-1 tracked the occurrence of single event upsets (SEU), finding the majority occurred while passing the inner belt during solar maximum and were likely caused by high energy protons.[6] The whole weight of the satellite was 480 kg.[1]
Japanese space program | |||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| |||||||||||||
Astronomical observation |
| ||||||||||||
Communications, broadcasting and navigation |
| ||||||||||||
Earth observation |
| ||||||||||||
Engineering tests |
| ||||||||||||
Human spaceflight |
| ||||||||||||
Lunar and planetary exploration |
| ||||||||||||
Private miniaturized satellites |
| ||||||||||||
Reconnaissance |
| ||||||||||||
|
← 2001 · Orbital launches in 2002 · 2003 → | |
---|---|
USA-164 | INSAT-3C | Tsubasa · DASH · VEP-3 | HESSI | Iridium 90 · Iridium 91 · Iridium 94 · Iridium 95 · Iridium 96 | EchoStar VII | Intelsat 904 | Kosmos 2387 | Envisat | STS-109 | TDRS-9 | GRACE | Progress M1-8 | Shenzhou 3 | JCSAT-8 · Astra 3A | Intelsat 903 | Kosmos 2388 | STS-110 (ITS S0) | NSS-7 | Soyuz TM-34 | SPOT-5 · Idefix | Aqua | DirecTV-5 | Feng Yun 1D · Hai Yang 1A | Ofek-5 | Kosmos 2389 | Intelsat 905 | STS-111 (Leonardo MPLM) | Ekspress A1R | Galaxy 3C | Iridium 97 · Iridium 98 | NOAA-17 | Progress M-46 | CONTOUR | Stellat 5 · N-STAR c | Kosmos 2390 · Kosmos 2391 | Kosmos 2392 | Hot Bird 6 | EchoStar VIII | Atlantic Bird 1 · MSG-1 | Intelsat 906 | USERS · Kodama | METSAT | Tsinghua 2 | Hispasat 1D | Progress M1-9 | Nadezhda 7 | STS-112 (ITS S1) | Foton-M No.1 | INTEGRAL | Zi Yuan 2B | Soyuz TMA-1 | Eutelsat W5 | STS-113 (ITS P1 · MEPSI 1A · MEPSI 1B) | Astra 1K | AlSAT-1 · Mozhayets 3 · Rubin-3 | TDRS-10 | Hot Bird 7 · Stentor · MFD-A · MFD-B | ADEOS II · Kanta Kun · FedSat · µ-LabSat 1 (RITE 1 · RITE 2) | NSS-6 | TrailBlazer-2001 STA · Saudisat 1C · LatinSat A · LatinSat B · UniSat 2 · Rubin 2 | Kosmos 2393 | Kosmos 2394 · Kosmos 2395 · Kosmos 2396 | Shenzhou 4 | Nimiq 2 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
![]() | This article about one or more spacecraft of Japan is a stub. You can help Wikipedia by expanding it. |