Shi gian
Thực tiễn Shíjiàn | |
Program overview | |
---|---|
Country | People's Republic of China |
Organization | China Academy of Space Technology(CAST) |
Purpose | Unknown, varied |
Status | Active |
Program history | |
Duration | 1971–present |
First flight | 3 March 1971 |
Last flight | 8 January 2023 |
Successes | 37 |
Failures | 5 |
Launch site(s) | |
Vehicle information | |
Launch vehicle(s) |
Shi gian(simplified Chinese:Thực tiễn;traditional Chinese:Thực tiễn;pinyin:Shíjiàn;lit.'Practice',abbr."SJ" ) is a series of satellites built and operated by thePeople's Republic of China.Some Shi gian -series satellites have drawn significant concerns from the United States government and space observers who cite unannounced launches, undisclosed sub-satellites deployed in orbit, unusual orbital maneuvers, and demonstrated rendezvous proximity operations (RPO) including the close inspection and towing of other satellites.[1][2][3][4]
Little is known about the series and what differentiates it from other experimental satellite series launched by China such as the Chuangxin (Chinese:Sáng tạo;pinyin:Chuàngxīn;lit.'Innovation') series or Shiyan (Chinese:Thực nghiệm;pinyin:Shíyàn;lit.'Experiment') series.[5]TheChina Aerospace Studies Instituteof theUnited States Air Forceasserts thatShiyan-series satellitesplay an earlier role in the systems development process testing various new technologies on a single bus while Shijan-series satellites are used to develop operational best practices and optimize the technologies previously tested on Shiyan-series satellites.[6]In this regard, "Shi gian" should be translated as "best practice", or "put into practice" while "Shiyan" ought to be translated as "experiment", "pilot", or "trial".
Notable satellites
[edit]Shi gian -17
[edit]Launched intogeostationary orbitaboard aLong March 5rocket on 3 November 2016 fromWenchang Space Launch Site,Shi gian -17 is the first Chinese satellite to bear a robotic arm. Observers question the robotic arm'sdual-purposesforspace debriscleanup andkinetic attacksagainst adversary satellites.[7][8][9]
In an April 2021 written statement to theUS Senate Armed Services Committee,GeneralJames H. Dickinson,Commander ofUnited States Space Command(USSPACECOM) was the first US official to speak publicly on Shi gian -17 warning of its counterspace capabilities. General Dickinson wrote "Beijingactively seeks space superiority through space and space attack systems. One notable object is the Shi gian -17, a Chinese satellite with a robotic arm. Space-based robotic arm technology could be used in a future system for grappling other satellites. "[10]
Shi gian -17 has also prompted concern among observers who have tracked Shi gian -17's uniqueorbital maneuvers.Since its launch, Shi gian -17 has occupied a wide span of orbital positions within itsgeostationary orbitto dynamically adjust its position relative to neighboring satellites. These varied positions have ranged from 37.7°E overAfricato 180°E over theMarshall Islands,uncharacteristic of other satellites designed for communications. Shi gian -17 has also positioned itself as close as 55 kilometers to other satellites for periods of a week or more while other geostationary satellites maintain an average 207-kilometer separation distance.[11][12][13]
Shi gian -17's robotic arm also earned mentions in the U.S. Office of the Secretary of Defense's congressionally-mandatedAnnual Report to Congress:Military and Security Developments involving the People's Republic of China.[14]The 2022 report, the first to mention Shi gian satellites by name, announced "The Shi gian -17 is a Chinese satellite with a robotic arm. Space-based robotic arm technology could be used in a future system for grappling other satellites."[14]The 2023 report specified "The Shi gian -17 was the PRC's first satellite with a robotic arm, technology that could be used in a future system for grappling adversary satellites."[15]
Shi gian -18
[edit]Shi gian -18 was a Chinese communications and technology demonstration satellite developed and launched by theChina Academy of Space Technologyon 2 July 2017. It was the maiden flight of the DHF-5 satellite bus, which is designed with 16-year lifespan. Shi gian -18 carried 18 experiments on board involving communications and space telescopes. It was lost after a malfunction on theLong March 5rocket carrying the satellite. It would have been the heaviest geostationary satellite at the time of its launch,[16]with a launch mass of 7,600 kg (16,800 lb). The satellite incorporated a high-thrustion propulsionsystem, a large trussed structure and a higher payload capacity.[17]More specifically, it used the LIPS-300xenon thrusterfororbit keeping,developed by the Lanzhou Institute of Physics. It was planned for the LIPS-300 system to be fully certified in this mission so that it could be used for geostationary and deep-space operations. The satellite would operate at theKa bandwith 70 Gb/s capacity, capable of providingbroadband internetto whole mainland China.[18]
Shi gian -18 launched from theWenchang Space Launch Siteon 2 July 2017 at 11:23UTCon board a Long March 5 rocket to a geostationary orbit. It was the rocket's second flight, the first being to launch Shi gian -17.[19]The rocket encountered an anomaly shortly after launch, causing it to switch into a gentler trajectory. However, 45 minutes into the flight, it was declared a failure, with the loss of the payload.[20][21]The cause of the failure was later determined to be a faulty oxidizer turbopump, which has now been redesigned twice.[22]The rocket and payload crashed in the Pacific Ocean somewhere at thePhilippine Sea.[23]
Shi gian -21
[edit]In October 2021, China launched Shi gian 21 (SJ-21) from Xichang Space Launch Center (XSLC) aboard a Long March 3B rocket into geosynchronous transfer orbit (GTO). Atypically, China issued no notifications prior to the launch confirming only after the satellite's successful launch.[24]China's official state news media organization, Xinhua News Agency, described SJ-21 as an On-Orbit Service, Assembly, and Manufacturing (OSAM) satellite that would be "mainly used to test and verify space debris mitigation technologies."[25][26][27]
A month after its launch, SJ-21 drew some suspicion from space observers as an object, described to be an undeclared sub-satellite, began orbiting closely alongside SJ-21 shortly after its entry intogeosynchronous orbit(GEO). The object was initially cataloged as an apogee kick motor (AKM) by theUS Space Force's18th Space Defense Squadron(SDS), however many doubt that a discarded motor would maintain the constant and proximate orbit with SJ-21 instead of gradually drifting away. SJ-21 drew further suspicion in January 2022 when, according to commercial space monitoring firm ExoAnalytic Solutions, SJ-21 went "missing" from itsorbital slotto dock with defunctBeidouG2 (Compass G2)navigation satellitecapitalizing on the inability of optical satellites to track space-objects during the day. Shi gian -21 then moved to an orbit 3,000 kilometers higher where it released the Beidou G2 satellite intograveyard orbitand returned to GEO.[28][29][30]
Many observers suspect the spacecraft, like many of China'sYaoganandGaofensatellites, serve primarily military purposes under the cover of more mundane missions.[31][32]With SJ-21's demonstrate capability to tug satellites from their orbit and China's increasing interest in space power, the spacecraft likely also offers the Chinese government a tool for counterspace operations.[25][26][33][29]Victoria Samson, the Washington Office director for theSecure World Foundationsaid "You could look at China working to develop the capability to remove inactive satellites on orbit as a way in which it is being a responsible space actor and cleaning up debris that it caused. Or you could use the lens that a lot of the US-based China watchers use and say that this could indicate that China is developing an on-orbit offensive capability."[29][34]Samson also praised commercial space situational awareness (SSA) providers for presenting the public and academia with satellite tracking capabilities previously exclusive to government.[29]China received criticism for its lack of transparency on Shi gian -21's operations.[29]
First mentioned by name in the 2022China Military Power Report,the U.S. Office of the Secretary of Defense writes "China has launched multiple satellites to conduct scientific experiments on space maintenance technologies and is conducting research on space debris cleanup; the most recent launch was the Shi gian -21 launched intoGEOin October 2021. In January 2022, Shi gian -21 moved a derelict BeiDou navigation satellite into a high graveyard orbit above GEO. "[14]The 2023 report restated the same.[15]
Satellites
[edit]Name | Launch | Function | Orbit | Orbital apsis | Inclination | SCN | COSPARID | Launch site | Launcher | Status |
---|---|---|---|---|---|---|---|---|---|---|
Shi gian 1 | 3 March 1971 | Particle measurements ofcosmic rays[35] | LEO | 266 km × 1826 km | 69.9° | 5007 | 1971-018A | JSLC | Long March 1 | Decayed |
Shi gian 2 | 19 September 1981 | Space dust/debris andEMstudy[35] | LEO | 232 km × 1598 km | 59.4° | 12845 | 1981-093D | JSLC | Feng Bao 1 | Decayed |
Shi gian 2A | 19 September 1981 | Space dust/debris andEMstudy[35] | LEO | 232 km × 1615 km | 59.4° | 12843 | 1981-093B | JSLC | Feng Bao 1 | Decayed |
Shi gian 2B | 19 September 1981 | Space dust/debris andEMstudy[35] | LEO | 232 km × 1608 km | 59.4º | 12842 | 1981-093A | JSLC | Feng Bao 1 | Decayed |
Shi gian 3 | N/A | Earth observation[36][37][38] | Cancelled, replaced byCBERS ZY-1[36] | |||||||
Shi gian 4 | 8 February 1994 | Space radiation monitoring[39][35] | HEO | 210 km × 36125 km | 28.6º | 22996 | 1994-010A | XSLC | Long March 3A | Decayed |
Shi gian 5 | 10 May 1999 | Test new minisatellite platform, particle measurement[35] | SSO | 569 km × 849 km | 98.8° | 25731 | 1999-025B | TSLC | Long March 4B | Decayed |
Shi gian 6-01B | 8 September 2004 | Space environment monitoring orELINT[40] | SSO | 585.4 km × 585.2 km | 97.7° | 28414 | 2004-035B | TSLC | Long March 4B | Operational |
Shi gian 6-01A | 8 September 2004 | Space environment monitoring orELINT[40] | SSO | 579.8 km × 596.7 km | 97.7° | 28413 | 2004-035A | TSLC | Long March 4B | Operational |
Shi gian 6-02A | 23 October 2006 | Space environment monitoring orELINT[40] | SSO | 591.0 km × 593.4 km | 97.8° | 29506 | 2006-046B | TSLC | Long March 4B | Operational |
Shi gian 6-02B | 23 October 2006 | Space environment monitoring orELINT[40] | SSO | 583.1 km × 587.7 km | 97.8° | 29505 | 2006-046A | TSLC | Long March 4B | Operational |
Shi gian 6-03A | 25 October 2008 | Space environment monitoring orELINT[40] | SSO | 576.5 km × 599.1 km | 97.8° | 33409 | 2008-053B | TSLC | Long March 4B | Operational |
Shi gian 6-03B | 25 October 2008 | Space environment monitoring orELINT[40] | SSO | 573.9 km × 600.1 km | 97.9° | 33408 | 2008-053A | TSLC | Long March 4B | Operational |
Shi gian 6-04A | 6 October 2010 | Space environment monitoring orELINT[40] | SSO | 585.9 km × 600.1 km | 97.8° | 37180 | 2010-051B | TSLC | Long March 4B | Operational |
Shi gian 6-04B | 6 October 2010 | Space environment monitoring orELINT[40] | SSO | 570.6 km × 606.8 km | 97.8° | 37179 | 2010-051A | TSLC | Long March 4B | Operational |
Shi gian 6-05A | 10 December 2021 | Space environment monitoring orELINT[40] | SSO | 467.5 km × 475.4 km | 97.3° | 49961 | 2021-122A | JSLC | Long March 4B | Operational |
Shi gian 6-05B | 10 December 2021 | Space environment monitoring orELINT[40] | SSO | 467.5 km × 475.4 km | 93.9° | 49962 | 2021-122B | JSLC | Long March 4B | Operational |
Shi gian 7 | 5 July 2005 | Unknown | SSO | 557.4 km × 605.5 km | 97.7° | 28737 | 2005-024A | JSLC | Long March 2D | Operational |
Shi gian 8 | 9 September 2006 | Space agricultural experiments[41] | LEO | 177 km × 445 km | 63.0° | 29385 | 2006-035A | JSLC | Long March 2C | Decayed |
Shi gian 9A | 14 October 2012 | Optical imaging, environmental monitoring[42] | SSO | 622 km × 647 km | 98.0° | 38860 | 2012-056A | TSLC | Long March 2C | Operational |
Shi gian 9B | 14 October 2012 | Optical imaging, environmental monitoring,LWIR[42] | SSO | 623 km × 649 km | 97.99° | 38861 | 2012-056B | TSLC | Long March 2C | Operational |
Shi gian 10 | 5 April 2016 | Retrievable microgravity experiments[43] | LEO | 234 km × 268 km | 42.89° | 41448 | 2016-023A | JSLC | Long March 2D | Decayed |
Shi gian 11-01 | 12 November 2009 | Launch warning,IRtracking[44] | SSO | 689.7 km × 708.1 km | 97.9° | 36088 | 2009-061A | JSLC | Long March 2C | Operational |
Shi gian 11-02 | 29 July 2011 | Launch warning,IRtracking[44] | SSO | 678.5 km × 701.3 km | 98.4° | 37765 | 2011-039A | JSLC | Long March 2C | Operational |
Shi gian 11-03 | 6 July 2011 | Launch warning,IRtracking[44] | SSO | 689.8 km × 704.1 km | 97.8° | 37730 | 2011-030A | JSLC | Long March 2C | Operational |
Shi gian 11-04 | 18 August 2011 | Launch warning,IRtracking[44] | (Launch Failure) | JSLC | Long March 2C | Payload lost in rocket failure[45] | ||||
Shi gian 11-05 | 15 July 2013 | Launch warning,IRtracking[44] | SSO | 689.4 km × 703.3 km | 98.2° | 39202 | 2013-035A | JSLC | Long March 2C | Operational |
Shi gian 11-06 | 31 March 2014 | Launch warning,IRtracking[44] | SSO | 692.3 km × 713.6 km | 98.1° | 39624 | 2014-014A | JSLC | Long March 2C | Operational |
Shi gian 11-07 | 28 September 2014 | Launch warning,IRtracking[44] | SSO | 690.6 km × 706.3 km | 98.1° | 40261 | 2014-059A | JSLC | Long March 2C | Operational |
Shi gian 11-08 | 27 October 2014 | Launch warning,IRtracking[44] | SSO | 685.0 km × 701.7 km | 98.2° | 40286 | 2014-066A | JSLC | Long March 2C | Operational |
Shi gian 12 | 15 June 2010 | Scientific research[46] | SSO | 575 km × 599 km | 97.68° | 36596 | 2010-027A | JSLC | Long March 2D | Operational |
Shi gian 13 | 12 April 2017 | High-throughput communications[47][48][49] | GEO | 35,765.3 km × 35,823.8 km | 0.1° | 42662 | 2017-018A | XSLC | Long March 3B | Operational |
Shi gian 15 | 19 July 2013 | Unknown payload deployment[50] | SSO | 670.6 km × 678.4 km | 98.0° | 39210 | 2013-037C | TSLC | Long March 4C | Operational |
Shi gian 16-01 | 25 October 2013 | Space environment monitoring orSIGINT[51][52] | LEO | 599 km × 616 km | 74.98° | 39358 | 2013-057A | JSLC | Long March 4B | Operational |
Shi gian 16-02 | 29 June 2016 | Space environment monitoring orSIGINT[51][52] | LEO | 596 km × 616 km | 75.00° | 41634 | 2016-043A | JSLC | Long March 4B | Operational |
Shi gian 17 | 3 November 2016 | Communications and debris inspection or counterspace[53] | GEO | 35,827.1 km × 35,835.4 km | 2.2° | 41838 | 2016-065A | WSLC | Long March 5 | Operational |
Shi gian 18 | 2 July 2017 | Test of new DFH-5 platform, telecom[54] | (Launch Failure) | WSLC | Long March 5 | Payload lost in rocket failure[55] | ||||
Shi gian 19 | TBA | Returnable microgravity experiments[56][57] | Planned: not yet launched | JSLC | Long March 2D | Planned | ||||
Shi gian 20 | 27 December 2019 | Test of new DFH-5 platform, experimental quantum telecom[58][59] | GEO | 35,774.9 km × 35,814.1 km | 1.347° | 44910 | 2019-097A | WSLC | Long March 5 | Operational |
Shi gian 21 | 24 October 2021 | Debris clean-up or counterspace[60][61] | GEO | 36,217.7 km × 36,217.7 km | 8.580° | 49330 | 2021-094A | XSLC | Long March 3B | Operational |
Shi gian 21 (subsat) | 24 October 2021 | Unknown[61][62] | 49382 | 2021-094C | XSLC | Long March 3B | Operational | |||
Shi gian 23 | 8 January 2023 | Classified | GEO | 35,769.1 km × 35,816.8 km | 0.6° | 55131 | 2023-002A | WSLC | Long March 7A | Operational |
Shi gian 23 (subsat) | 8 January 2023 | Unknown[63] | 55180 | 2023-002C | WSLC | Long March 7A | Operational | |||
Sources:NORAD,NASA,USSPACECOM,Celestrak,Gunter's Space Page |
See also
[edit]References
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