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SHENZHOU-9 (SZ-9) (38461)
COSPAR: 2012-032A | Alt Name: Shenzhou 9
DECAYED
Image
Additional Sources
Launch Details
Launch Date
June 16, 2012
Launch Site
JSC
Launch Pad
LC921
Launch Vehicle
Chang Zheng 2F
Orbital Elements
NORAD ID
38461
International Designator
2012-032A
Decay Date
6/29/2012
Basic Satellite Info
Name
SHENZHOU-9 (SZ-9)
Alternative Name
Shenzhou 9
Type
Payload
Status
Decayed
Owner
CMSEO
Country
China
Constellation
N/A
Related Satellites
Major Events
N/A
Summary
SHENZHOU-9 (SZ-9), also known as Shenzhou 9, is a crewed spacecraft launched by China on June 16, 2012, from the Jiuquan Satellite Launch Center using a Chang Zheng 2F launch vehicle. The spacecraft measures 9.3 meters in length and has a diameter of 3.2 meters with a span of 17 meters. It consists of a service module, return module, and an orbital module equipped with a docking collar. SHENZHOU-9 features two deployable solar arrays and batteries for power supply and is configured to support crewed missions. The satellite's dry mass and launch mass are both recorded as 3240 kg, indicating it was launched without additional payload or propellant beyond its operational weight. Its shape consists of a cylindrical body with two panels, and the spacecraft was manufactured by CALT for the China Manned Space Engineering Office (CMSEO). The mission purpose is to conduct crewed space missions, equipped with 4 retro motors for re-entry maneuvers.
Physical Characteristics
Length
9.3
Diameter
3.2
Span
17
Dry Mass
3240
Launch Mass
3240
Shape
Cyl + 2 pan
Radar Cross Section
0.3407
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Shenzhou 9 Fanhui Cang
Purpose
Crewed spacecraft
Mission
Crewed spacecraft
Manufacturer
CALT
Life Expectancy
Unknown
Bus
Shenzhou
Configuration
Service module, Return module, orbital Module with docking collar
Motor
4 x retro motors
Equipment
Unknown
Power System
2 deployable solar arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
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