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Long March 4B

The Long March 4B, also known as the Chang Zheng 4B, CZ-4B, and LM-4B, is a Chinese expendable orbital launch vehicle. Launched from Launch Complex 1 at the Taiyuan Satellite Launch Center, it is a 3-stage launch vehicle, used mostly to place satellites into low Earth orbit and Sun-synchronous orbits. It was first launched on 10 May 1999, with the FY-1C weather satellite, which would later be the target in the 2007 Chinese anti-satellite missile test.
The Chang Zheng 4B experienced its only launch failure on 9 December 2013, with the loss of the CBERS-3 satellite.

Characteristics:

Heigth: 47.2 meters
Mass: 249 Tons
Payload to GTO: 1.5 Tons

CBERS-1

China-Brazil Earth Resources Satellite-1 was a remote sensing satellite which was operated as part of the China–Brazil Earth Resources Satellite program between the China National Space Administration and Brazil's National Institute for Space Research. The first CBERS satellite to fly, it was launched by China in 1999

CBERS-1 was a 1,450 kg (3,200 lb) spacecraft built by the China Academy of Space Technology and based on the Phoenix-Eye 1 satellite bus. The spacecraft was powered by a single solar array, providing 1,100 watts of electricity for the satellite's systems. The instrument suite aboard the CBERS-1 spacecraft consisted of three systems: the Wide Field Imager (WFI) produced visible-light to near-infrared images with a resolution of 260 metres (850 ft) and a swath width of 890 km (550 mi); a high-resolution CCD camera was used for multispectral imaging at a resolution of 20 metres (66 ft) with a swath width of 113 km (70 mi); the third instrument, the Infrared Multispectral Scanner (IMS), had a resolution of 80 metres (260 ft) and a swath width of 120 kilometres (75 mi).

GENERAL INFO

  • Predecessor: CZ-3B/E
  • Successors 1 craft(s)
  • Created On: Android
  • Game Version: 1.3.204.1
  • Price: $16,155k
  • Number of Parts: 202
  • Dimensions: 47 m x 5 m x 5 m

PERFORMANCE

  • Total Delta V: 12.0km/s
  • Total Thrust: 4.7MN
  • Engines: 14
  • Wet Mass: 2.51E+5kg
  • Dry Mass: 18,069kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 4 3.8km/s 3.3MN 2.6m 2.51E+5kg
2 4 16m/s 414kN 2s 53,213kg
3 5 3.2km/s 883kN 2.1m 53,213kg
7 1 5.0km/s 102kN 6.1m 15,399kg

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