[1] SKUHERSKY M, GO T, KIRK D R, et al.. Comparison of propellant settling approaches for on-orbit propellant depots during propellant transfer maneuvers［C］. AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019 AIAA 2019-1371: 1-16.
[2] GAJJAR P, MALHOTRA V. Advanced upper stage energetic propellants［C］.2018 IEEE Aerospace Conference, March 3-10, 2018. Big Sky, MT. New York, USA: IEEE, 2018: 1-12.
[3] BARBER T J. Final cassini propulsion system in-flight characterization［C］.2018 Joint Propulsion Conference, Cincinnati, Ohio. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018, AIAA 2018-4546: 1-81.
[4] LEVERONE F, CERVONE A, GILL E. Cost analysis of solar thermal propulsion systems for microsatellite applications［J］. Acta Astronautica, 2019, 155: 90-110.
[5] HOPKINS J R, MICCI M M, BILEN S G, et al.. Direct thrust measurements of an 8-GHz microwave electrothermal thruster［J］. IEEE Transactions on Plasma Science, 2018, 46(6): 2009-2015.
[6] VAIRAMANI M, DURAISAMY V V, KULKARNI M D, et al.. Stability analysis of a novel on-orbit propellant storage and transfer system［C］. 2018 Space Flight Mechanics Meeting, Kissimmee, Florida. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018 AIAA 2018-0210: 1-15.
[7] GREGORY T C, GRAHAM K W, MARCOS R E, et al.. Restore-L propellant transfer subsystem progress within SSPD［C］. AIAA Propulsion and Energy Forum, Cincinnati, Ohio, 2018, AIAA 2018-4942: 1-17.
[8] CONOMOS H A, ALONGI C G, MOORE J, et al.. Development of 10 inch diameter titanium rolling metal diaphragm tank for green propellant［C］.53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, GA. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017-4915: 1-10.
[9] NAUMANN K W, PINTO P C. Green, controllable, safe, affordable and mature gelled propellant rocket motor technology for space and sub-orbital launchers［C］. 2018 Joint Propulsion Conference, Cincinnati, Ohio. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018-4854: 1-13.
[10] BOURDELLE A, BURLION L, BIANNIC J M, et al.. Correction: towards new controller design oriented models of propellant sloshing in observation spacecraft［C］. AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019-0115: 1-12.
[11] HARI M, SARIGUL-KLIJN N. Predicting sloshing motion in flexible propellant tanks using three-dimensional computational simulation and experimental validation［C］. AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019-0204: 1-10.
[12] OTTANDER J A, HALL R A, POWERS J F. Practical methodology for the inclusion of nonlinear slosh damping in the stability analysis of liquid-propelled space vehicles［C］.2018 AIAA Guidance, Navigation, and Control Conference, Kissimmee, Florida. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018-2097: 1-13.
[13] DONO A, PLICE L, MUETING J, et al.. Propulsion trade studies for spacecraft swarm mission design［C］.2018 IEEE Aerospace Conference, March 3-10, 2018. Big Sky, MT. New York, USA: IEEE, 2018: 1-12.
[14] XAPSOS M. A brief history of space climatology: from the big bang to the present［J］. IEEE Transactions on Nuclear Science, 2019, 66(1): 17-37.
[15] GRANT B, LUKE S. A new approach to radiation tolerance for high-orbit and interplanetary smallsat missions［C］. 32nd Annual AIAA/USU Conference on Small Satellites, Logan, Utah, 2018, SSC18-WKV-05: 1-12.
[16] XU F X. Technique of successful rescue of FY-1B meterological satellite by using the geomagnetic field and the gravitational field［J］. Journal of Astronautics, 2001, 22(2): 1-11, 17. (in Chinese)
[17] PENG R J, MA X Y, ZHENG K Y, et al.. On-orbit fault repair and recovery of a low orbit satellite［J］. Spacecraft Engineering, 2008, 17(1): 24-29. (in Chinese)
[18] SCHNEIDER P, ENDICTER J, WORK K, et al.. GOES-12 B-string thruster leak - anomaly response, recovery, and maintenance［C］.SpaceOps 2010 Conference, Huntsville, Alabama. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010-2140: 1-11.
[19] VAREHA A. The ISS 2B PVTCS ammonia leak: an operational history［C］.SpaceOps 2014 Conference, Pasadena, CA. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014-1664: 1-11.
[20] CHRISTIAN B, FLAVIO M, MILAN K, et al.. Propellant gauging experience with meteosat second generation S/C fleet［C］. Space Ops. 2018 Conference, Marseille, France, 2018, AIAA 2018-2319: 1-11.
[21] CARLTON A, MORGAN R, LOHMEYER W, et al.. Telemetry fault-detection algorithms: applications for spacecraft monitoring and space environment sensing［J］. Journal of Aerospace Information Systems, 2018, 15(5): 239-252.
[22] MLLER S, GERNDT A, NOLL T. Synthesizing failure detection, isolation, and recovery strategies from nondeterministic dynamic fault trees［J］. Journal of Aerospace Information Systems, 2019, 16(2): 52-60.
[23] BUSSY-VIRAT C D, RIDLEY A J, GETCHIUS J W. Effects of uncertainties in the atmospheric density on the probability of collision between space objects［J］. Space Weather, 2018, 16(5): 519-537.
[24] HEJDUK M D, SNOW D E. The effect of neutral density estimation errors on satellite conjunction serious event rates［J］. Space Weather, 2018, 16(7): 849-869.
[25] LIM J W M, HUANG S Y, SUN Y F, et al.. Precise calibration of propellant flow and forces in specialized electric propulsion test system［J］. IEEE Transactions on Plasma Science, 2018, 46(2): 338-344.
[26] LI Q, LI H F, YUAN Y, et al.. Estimation for cold gas propellant leakage on orbit［J］. Journal of Propulsion Technology, 2018, 39(5): 1187-1193. (in Chinese)
[27] ZONG Y H, YU Y B, DI J J, et al.. High precision time correction and calculation method of star camera［J］. Spacecraft Engineering, 2019, 28(2): 36-42. (in Chinese)
[28] VANHOVE E, ROUSSEL J F, REMAURY S, et al.. Aging of thermal coatings on low earth orbit: in-flight measurements and modeling［J］. Journal of Spacecraft and Rockets, 2016, 53(6): 1141-1145.
[29] ZHOU X, ZHANG Y W, YU L, et al.. Experimental study of the long-term compatibility of superalloy GH4169 with dinitrogen tetroxide［J］. Spacecraft Environment Engineering, 2019, 36(2): 161-164. (in Chinese)
[30] DANIELS C C, BRAUN M J, ORAVEC H A, et al.. Leak-rate-quantification method for gas pressure seals with controlled pressure differential［J］. Journal of Spacecraft and Rockets, 2017, 54(6): 1228-1234.
[31] TAYLOR S C, MATHER J, DANIELS C C. Investigation of the impact of surface blending and ultraviolet radiation exposure on elastomer seal leak rate performance for space seal applications［C］.7th AIAA Atmospheric and Space Environments Conference, Dallas, TX. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015-3322: 1-11.
[32] DANIELS C, WASOWSKI J, PANICKAR M, et al.. Leak rate performance of three silicone elastomer compounds after ground-simulated and on-orbit environment exposures［C］.3rd AIAA Atmospheric Space Environments Conference, Honolulu, Hawaii. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011-3823: 1-11.
[33] PENNEY N, WASOWSKI J, DANIELS C. Temperature and atomic oxygen effects on helium leak rates of a candidate main interface seal［C］.46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, TN. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010-6986: 1-7.
[34] JIA SH J, MING ZH P, LIU J Y, et al.. Analysis on the thermal control problems of space booster sub-system in orbit［J］.Spacecraft Environment Engineering,2019,36(2): 165-170. (in Chinese)
[35] IOVINE J. International space station passive thermal control system top ten lessons-learned［C］. 48th International Conference on Environmental Systems, Albuquerque, New Mexico, 2018, ICES-2018-004: 1-8.
[36] CHAMBLISS J. The ISS TCS system manager experience［C］. 48th International Conference on Environmental Systems, Albuquerque, New Mexico, 2018, ICES-2018-297: 1-16.
[37] BUHL N, ALTENBURG M, MANNS M. Sentinel-2A/B thermal design-lessons learnt from TBTV, LEOP and IOC［C］. 48th International Conference on Environmental Systems, Albuquerque, New Mexico, 2018, ICES-2018-148: 1-16.
[38] YANG B H. Exploration of CASC′s commercial space［J］. Aerospace China, 2018, 19(1): 27-30.
[39] WANG S, JIN R, ZHU J D. SuperView-1 - China′s first commercial remote sensing satellite constellation with a high resolution of 0.5 m［J］. Aerospace China, 2018, 19(1): 31-38.
[40] YOU ZH, SHI SH, ZHAO K CH, et al.. Key technologies for research & development of nanosatellite［J］. Spacecraft Engineering, 2019, 28(1): 1-9. (in Chinese)
[41] BAI ZH G. Development achievements and prospects of China modern small satellite［J］. Spacecraft Engineering, 2019, 28(2): 1-8. (in Chinese)
