Lancement CZ-2D | GF-9 à JSLC - le 14 Septembre 2015 [Succès]

David L. a écrit:Quel est le décalage horaire avec la France ?

Elixir a écrit:

David L. a écrit:Quel est le décalage horaire avec la France ?

Heure de Pékin = Heure de Paris + 6h, actuellement.

Henri K.

A2591/15 NOTAMN
Q) ZLHW/QRTCA/IV/BO/W/000/999/3524N09839E018
A) ZLHW B) 1509150435 C) 1509150457
E) A TEMPORARY RESTRICTED AREA ESTABLISHED BOUNDED BY:
N350835E0984113-N351211E0982201-N354113E0983025-N353629E0985613
BACK TO START. VERTICAL LIMITS:GND-UNL.
F) GND G) UNL

A2609/15 NOTAMN
Q) ZLHW/QRTCA/IV/BO/W/000/999/3524N09839E018
A) ZLHW B) 1509140435 C) 1509140457
E) A TEMPORARY RESTRICTED AREA ESTABLISHED BOUNDED BY:
N350835E0984113-N351211E0982201-N354113E0983025-N353629E0985613
BACK TO START. VERTICAL LIMITS:GND-UNL.
F) GND G) UNL

Elixir a écrit:


Henri K.

Kitu a écrit:

Sur cette photo on voit une fumée rouge qui sort du lanceur sur son côté à la moitié du 1° étage, c'est quoi ??  :???:  et surtout, est-ce normal ?

2015-047A
1 40894U 15047A 15257.24064233 -.00000054 00000-0 00000+0 0 9995
2 40894 98.0079 337.7600 0033917 250.0392 109.7164 14.76427326 00

CAST3000 Bus

The CAST3000 is a top class small satellite bus characterized by its high precision, high agility, high automatization, prolonged life-span and high reliability, which can support both high resolution imaging and agile imaging missions. The bus can perform swift and wide range of attitude maneuver and have free space pointing capacity. It can realize multi-mode imaging
(including area target imaging, continuous strap imaging, composite straps imaging and single
orbit stereo imaging, etc). Also, it supports S/X data transmission and onboard highly effective
power supply; has the capability of automatic onboard mission management and scheduling; adopts a highly integrated onboard synthesized electronic system; and achieves a 50-60% carrying capacity and a more-than-5-year designed lifespan.

Technical Specifications

Bus mass: 300-400kg
Payload capacity: >380kg
Orbit type: low, medium and high orbits
Attitude control ability: 3-axis stabilization,
Pointing mode: earth pointing or inertial space pointing
Attitude maneuver ability: maneuver range: ±45° (along roll and pitch axes)
stereo speed: 5° within 11s, 15° within 16s,
30° within 21s, 45° within 25s, 60° within 30s,
90° within 35s(including stabilization time, along roll and pitch axes)
Attitude measurement accuracy: < 0.001° (3-axis@3σ);
Attitude pointing accuracy: < 0.05°(3-axis@3σ);
Attitude stability: < 0.0005°/s (3-axis@3σ)
Orbit control: hydrazine propellant: 32.5~130kg optional
Solar array output power: 945~1148W (EOL)
Designed lifetime: >5 years

Applications
The satellite bus can be widely applied in different missions, such as earth observation, technological demonstration, scientific exploration, earth environmental exploration, formation flight and networking, meteorological research and application, communications, navigation, and so on. And it is mainly applicable to the high resolution optical imaging and radar imaging missions.

高分九号作为我国首颗敏捷卫星，主要应用于国土普查、城市规划、土地确权、路网设计、农作物估产和防灾减灾等领域，可为“一带一路”建设等国家重大战略实施和国防现代化建设提供信息保障。

卫星与相机采用了多项新技术，从而实现了卫星快速机动、稳定成像的功能，相机可实现全色分辨率0.5米，多光谱分辨率2米。

508所还承担了高分四号、高分五号及高分七号相机的研制，高分专项形成的产品和产能可以被扩充装备到商业遥感系统中。高分型号的在轨成功应用，也为集团公司“16+4+4+X”商业遥感卫星星座的研制打下了良好的产品及技术基础。