Long March 3A
ActiveChina Aerospace Science and Technology Corporation (CASC)
Feb. 8, 1994
Description
Specifications
-
Minimum Stage
1 -
Max Stage
3 -
Length
52.5 m -
Diameter
3.35 m -
Fairing Diameter
― -
Launch Mass
240.0 T -
Thrust
2962.0 kN -
Apogee (Sub-Orbital)
40000.0 km
Family
-
Name
Long March 3A -
Family
― -
Variant
― -
Alias
― -
Full Name
Long March 3A
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
2300.0 kg -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
China Aerospace Science and Technology Corporation
Government
Chairman & President: Lei Fanpei
CASC 1999The China Aerospace Science and Technology Corporation (CASC) is the main contractor for the Chinese space program. It is state-owned and has a number of subordinate entities which design, develop and manufacture a range of spacecraft, launch vehicles, strategic and tactical missile systems, and ground equipment. It was officially established in July 1999 as part of a Chinese government reform drive, having previously been one part of the former China Aerospace Corporation. Various incarnations of the program date back to 1956.
Long March 3A | Beidou-2 I7
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July 9, 2018, 8:58 p.m.
Long March 3A | Fengyun-2H
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June 5, 2018, 1:07 p.m.
Long March 3A | Beidou No. 22
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March 29, 2016, 8:11 p.m.
Long March 3A | Fengyun 2-08
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Dec. 31, 2014, 1:02 a.m.
Long March 3A | Fengyun 2-07
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Jan. 13, 2012, 12:56 a.m.
Long March 3A | Compass-IGSO-5
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Dec. 1, 2011, 9:07 p.m.
Long March 3A | Compass-IGSO-4
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July 26, 2011, 9:44 p.m.
Long March 3A | Compass-IGSO-3
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April 9, 2011, 8:47 p.m.
Long March 3A | Compass-IGSO-2 (Compass-I2)
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Dec. 17, 2010, 8:20 p.m.
Long March 3A | ZhongXing-20A
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Nov. 24, 2010, 4:09 p.m.
Long March 3A | Compass-IGSO-1 ( BEIDOU-2 IGS-1)
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
July 31, 2010, 9:30 p.m.
Long March 3A | Feng Yun 2E
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Dec. 23, 2008, 12:54 a.m.
Long March 3A | Chang'e-1
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Oct. 24, 2007, 10:05 a.m.
Long March 3A | Xinnuo 3
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
May 31, 2007, 4:08 p.m.
Long March 3A | Beidou DW 1
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
April 13, 2007, 8:11 p.m.
Long March 3A | Beidou Daohang Shiyan Wei. 4
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Feb. 2, 2007, 4:28 p.m.
Long March 3A | Feng Yun 2D
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Dec. 8, 2006, 12:53 a.m.
Long March 3A | Zhongxing 22A
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Sept. 12, 2006, 4:02 p.m.
Long March 3A | Feng Yun 2C
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Oct. 19, 2004, 1:20 a.m.
Long March 3A | Zhongxing 20
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Nov. 14, 2003, 4:01 p.m.
Long March 3A | Beidou Daohang Shiyan Wei. 3
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
May 24, 2003, 4:34 p.m.
Long March 3A | Beidou Daohang Shiyan Wei. 2
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Dec. 20, 2000, 4:20 p.m.
Status: Launch Successful
Mission:
The BD 1 (Beidou 1) satellites were the 1st phase of the chinese Beidou (Compass) satellite navigation system. The first phase uses only geostationary satellites, in contrast to GPS and GLONASS. This reduces the number of satellites, but limits the coverage to a less than hemispherical area. The basic constellation requires 3 satellites. The satellites are based on the DFH-3 Bus.
Geostationary OrbitLong March 3A | Beidou Daohang Shiyan Wei.
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Oct. 30, 2000, 4:02 p.m.
Status: Launch Successful
Mission:
The BD 1 (Beidou 1) satellites were the 1st phase of the chinese Beidou (Compass) satellite navigation system. The first phase uses only geostationary satellites, in contrast to GPS and GLONASS. This reduces the number of satellites, but limits the coverage to a less than hemispherical area. The basic constellation requires 3 satellites. The satellites are based on the DFH-3 Bus.
Geostationary OrbitLong March 3A | Zhongxing 22
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Jan. 25, 2000, 4:45 p.m.
Long March 3A | Zhongxing 6
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
May 11, 1997, 4:17 p.m.
Status: Launch Successful
Mission:
The DFH-3 satellite is a medium-capacity geostationary communications satellite based on the DFH-3 Bus (three-axis-stabilized telecommunications satellite platform). The 2200 kg satellite carries 24 C-band transponders, providing six television channels and 18 communications transmission channels. It has a power supply of 2 kW and a design life of 8 years.
Geostationary OrbitLong March 3A | DFH-3
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Nov. 29, 1994, 5:02 p.m.
Status: Launch Successful
Mission:
The DFH-3 satellite is a medium-capacity geostationary communications satellite based on the DFH-3 Bus (three-axis-stabilized telecommunications satellite platform). The 2200 kg satellite carries 24 C-band transponders, providing six television channels and 18 communications transmission channels. It has a power supply of 2 kW and a design life of 8 years.
Geostationary OrbitLong March 3A | Shi Jian 4
China Aerospace Science and Technology Corporation | ChinaXichang Satellite Launch Center, People's Republic of China
Feb. 8, 1994, 8:33 a.m.
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