Dati principali del lancio
|
|
| Data di lancio |
2017-10-09 22:01:37 |
| Esito lancio |
SUCCESSO |
Dettagli della missione
|
|
| Nome |
Michibiki 4 (QZS-4) |
| 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36号機による準天頂衛星みちびき4号機の打上げを中継します。 打上げ予定日：2017年10月10日 打上げ予定時間帯：７時00頃（予定） 打上げ予備期間：2017年10月11日～11月30日 打上げ時刻は8日14時からの打上げ前会見 https://www.youtube.com/watch?v…
Altri video
Ultimo aggiornamento: 2022-07-01T03:49:01 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.
