SuperView duo launched by Long March 2D – Suffers problem

by Rui C. Barbosa

The first Long March 2D to launch from the Taiyuan Satellite Launch Center launched the first pair of a new civilian multi-sensor commercial remote sensing satellite constellation for China. However, the health of the spacecraft – not least their deployed orbit – is currently deemed to be problematic. The launch took place at 03:23 UTC on December 28 from the LC9 launch complex.

The Gaojing-1 remote sensing satellites:

Also known as SuperView-1, the Gaojing-1 is a satellite constellation for civilian remote sensing use that will be operated by the Siwei Star Co. Ltd., Beijing.

Siwei Star is the owner and operator of the constellation. It is held by China Siwei Surveying and Mapping Technology Co. Ltd., the subsidiary of China Aerospace and Technology Corporation (CASC). Beijing Space View Technology Co., Ltd. acts as the exclusive global distributor of the satellite data.

The constellation will comprise four satellites orbiting in the same orbital plane and at an altitude of 500 km.  The satellites will provide imagery with 0.5 m panchromatic resolution and 2 m multispectral resolution with a swath width of 12 km.

The satellites will operate with multiple collection modes including long strip, multiple strips collect, multiple point targets collect and stereo imaging. The maximum single scene can be 60 km × 70 km.

By the year 2022, the full constellation will be completed, comprising of 16+4+4+X multi-sensor commercial high-resolution satellite constellation with strong capability to provide data and services to clients across the world. The full constellation will have 16 optical satellites with 0.5 resolution, 4 satellites with resolution better than 0.5, 4 VHR X-band SAR satellites and multiple micro video and hyperspectral satellites.

The SuperView-1 constellation works in multiple modes, such as imaging at nadir, rolling imaging, long strip, multiple strips collect, multiple point targets collect and stereo imaging.

The multiple strips collect is able to realize high-resolution surveying and mapping with large swath width, and the stereo imaging mode will bring large opportunities for EDM production. The SuperView services will be totally commercial and will customize data collection services and develop derived products based on marketing demands.

The Gaojing-1 satellites are based on the CAST3000B satellite platform.

Together with the two Gaojing satellites, the Long March-2D orbited the small BY70-1 satellite. BY70-1 is a CubeSat-2U project led by China Center for Aerospace Science and Technology International Communications for school education and amateur radio.

The amateur radio station onboard will provide telecommand, telemetry and FM repeater functions. The spacecraft is 3 axis stabilized and has deployable solar panels. It will operate on a 530km circular SSO.

Launch Vehicle and Launch Site:

The Chang Zheng-2D launch vehicle is a two-stage rocket developed by the Shanghai Academy of Spaceflight Technology. With storable propellants is mainly used to launch a variety of low earth orbit satellites.

The development of CZ-2D was started in February 1990. From 2002, to meet the demand of SSO satellites, the payload fairing of 3350mm in diameter and attitude control engine for second stage have been successfully developed; and the discharge of remaining propellant and de-orbit of the second stage have been realized. This launcher is mainly used for launching LEO and SSO satellites. It is characterized by high reliability, wide application and mature technology.

The CZ-2D can launch a 1,300 kg cargo in a 645 km SSO. The rocket is 41.056m long and the first, second stages and payload fairing are all 3.35m in diameter.

Its first stage is the same of the CZ-4 Chang Zheng-4. The second stage is based on CZ-4 second stage with an improved equipment bay. Lift-off mass is 232,250 kg, total length 41,056 meters, diameter 3.35 meters and fairing length 6.983 meters. At launch it develops 2961.6kN engine thrust.

The first stage has a 27.910 meter length with a 3.35 meter diameter, consuming 183,200 kg of N2O4 / UDMH (launch mass of the first stage is 192,700 kg). Equipped with a YF-21C engine capable of a ground thrust of 2,961.6 kN and a ground specific impulse of 2,550 m/s. Burn time is 170 seconds.

The second stage has a 10.9 meter length with a 3.35 meter diameter, launch mass of 39,550 kg and consuming 45,550 kg of N2O4 / UDMH. Equipped with a YF-24C cluster engine with a main engine vacuum thrust of 742.04 kN and a vernier engine with a vacuum thrust of 47.1 kN (specific impulses of 2,942 m/s and 2,834 m/s, respectively).

The CZ-2D can use two types of fairings depending on the cargo. Type A fairing has a 2.90 meters diameter (total launch vehicle length is 37.728 meters) and Type B fairing with a diameter of 3.35 meters – total launch vehicle length is 41.056 meters.

The first launch of the CZ-2D was on August 9th, 1992 from the Jiuquan Satellite Launch Center orbiting the Fanhui Shei Weixing FSW-2-1 (22072 1992-051A) recoverable satellite.

The launch took place from the Taiyuan Satellite Launch Center (TSLC). Situated in the Kelan County in the northwest part of the Shanxi Province, TSLC is also known by the Wuzhai designation. It is used mainly for polar launches (meteorological, Earth resources and scientific satellites).

The launch center has two single-pad launch complexes, a technical area for rocket and spacecraft preparations, a communications center, a mission command and control center, and a space tracking center.

The stages of the rocket were transported to the launch center by railway and offloaded at a transit station south of the launch complex. They were then transported by road to the technical area for checkout procedures.

The launch vehicles were assembled on the launch pad by using a crane at the top of the umbilical tower to hoist each stage of the vehicle in place. Satellites were airlifted to the Taiyuan Wusu Airport about 300km away and then transported to the center by road.

The TT&C Centre, also known as Lüliang Command Post, is headquartered in the city of Taiyuan, It has four subordinate radar tracking stations in Yangqu (Shanxi), Lishi (Shanxi), Yulin (Shaanxi), and Hancheng (Shaanxi).

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