Dati principali del lancio
|
|
| Data di lancio |
2017-06-01 00:17:46 |
| Esito lancio |
SUCCESSO |
Dettagli della missione
|
|
| Nome |
Michibiki 2 (QZS-2) |
| Tipo |
Telecomunicazioni |
| Orbita |
Orbita geosincrona (GSO) |
Centro e rampa di lancio
|
|
|
| Nome |
Yoshinobu Launch Complex - Tanegashima, Giappone1 2
|
 |
| Lanci dalla rampa |
39 |
|
| Lanci dal Centro |
84 |
|
| Atterraggi al Centro |
0 |
|
Lanciatore
|
|
| Vettore |
H-IIA 202 1
|
| Costruttore |
Mitsubishi Heavy Industries 1 2
|
| Fornitore servizi di lancio |
Mitsubishi Heavy Industries 1 2
|
| Primo volo |
2001-08-29 |
| Numero stadi |
2 |
| Altezza |
53,00 m |
| Diametro |
4,00 m |
| Peso al lancio |
285 t |
| Spinta al decollo |
2.260 kN |
| Capacità di carico |
LEO: 10.000 kg
GTO: 4.100 kg |
| Successi/Lanci totali |
28/28 (28 consecutivi) |
Video
H-IIAロケット34号機による「みちびき2号機」打ち上げの様子をライブ中継した録画です。 打ち上げ時刻：9時17分46秒 放送時間：約35分 ＊時刻はいずれも予定です。 ＊番組は、打ち上げ準備の状況などにより、延期・時刻変更・休止、延伸・短縮する場合があります。その場合の代替番組はございません。 ＊授業など学校…
Altri video
Ultimo aggiornamento: 2022-07-01T03:59:00 con AstronautiBOT 10 beta 1 - Fonte: LaunchLibrary2 API
The Quasi-Zenith Satellite System (QZSS) is a three-satellite regional time transfer system and the satellite-based augmentation system for the GPS that would be receivable within Japan. The primary purpose of QZSS is to increase the availability of GPS in Japan’s numerous urban canyons, where only satellites at very high elevation can be seen. A secondary function is performance enhancement, increasing the accuracy and reliability of GPS derived navigation solutions. A single satellite weighs about 4000 kg, has an expected lifetime of 15 years and is put in a elliptical, highly inclined geosynchronous orbit.
