Development Analysis of Active Long-Term On-Orbit Cryogenic Propellant Boil-Off Control Technology

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  • 1. School of Aerospace Engineering,Tsinghua University,Beijing 100084,China;
    2. China Academy of Launch Vehicle Technology,Beijing 100076,China

Received date: 21 Feb 2017

Revised date: 01 Jun 2017

Abstract

To meet the requirements of deep space missions,the research progress of active long-term on-orbit cryogenic propellant boil-off control technology was analyzed based on its application requirements. The key technologies were introduced according to the technology development situation in China,which can provide some references to cryogenic launch system for deep space missions.

Cite this article

LIU Xin, ZHANG Xiaoyu . Development Analysis of Active Long-Term On-Orbit Cryogenic Propellant Boil-Off Control Technology[J]. Journal of Deep Space Exploration, 2017 , 4(3) : 203 -211 . DOI: 10.15982/j.issn.2095-7777.2017.03.001

References

[1] 胡伟峰,申麟,彭小波,等. 低温推进剂长时间在轨的蒸发量控制关键技术分析[J]. 低温工程,2011(3):59-66
Hu W F,Shen L,Peng X B,et al. Key technology analysis of boil-off control study on cryogenic propellant long-term application on orbit[J]. Cryogenics,2011(3):59-66
[2] 胡伟峰,申麟,杨建民,等. 低温推进剂长时间在轨的蒸发量控制技术进展[J]. 导弹与航天运载技术,2009(6):28-34
Hu W F,Shen L,Yang J M,et al. Progress of study on transpiration control technology for orbit long-term applied cryogenic propellant[J]. Missiles and Space Vehicles,2009(6):28-34
[3] Hastings L J,Plachta D W,Salerno L,et al. An overview of NASA efforts on zero boil-off storage of cryogenic propellants[J]. Cryogenics,2001,41(2002):833-839
[4] De Kruif J S,Kutter B F. Centaur upper stage applicability for several-day mission durations with minor insulation modifications[C]//43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Cincinnati,OH:AIAA,2007.
[5] Michael D,Kirk A,Bernard K. Design and development of an in-space deployable sun shield for the atlas centaur[C]//AIAA Space 2008 Conference & Exposition. San Diego,California:AIAA,2008.
[6] Plachta D W,Christie R J,Jurns J M,et al. ZBO cryogenic propellant storage applied to a Mars sample return mission concept[J]. Advances in Cryogenic Engineering:Transactions of the Cryogenic Engineering Conference. 2006,56:205-212
[7] Doherty M P,Gaby J D,Salerno L J,et al. Cryogenic fluid management technology for Moon and Mars missions[C]//AIAA SPACE 2009 Conference & Exposition. Pasadena,California:AIAA,2009.
[8] Kyle C,Sarah K,Justin K. Cryogenic fluid storage for the mission to Mars[D]. USA:Texas Tech University,1999.
[9] Nast T,Frank D. Cryogenic propellant boil-off reduction approaches[C]//49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Orlando,Florida:AIAA,2011.
[10] McLean C H,Mills G L,Riesco M E. Long term space storage and delivery of cryogenic propellants for exploration[C]//44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Hartford,CT:NASA,2008.
[11] Keller C W. Thermal performance of multilayer insulations[R]. USA:NASA,1974.
[12] Martin J J,Smith J W. Cryogenic testing of a foam-multilayer insulation concept in a simulated orbit hold environment [C]//AIAA/ASME/SAE/ASEE 29th Joint Propulsion Conference and Exhibit. Washington,D.C:AIAA,1993.
[13] Robert J S,Richard H K. Thermal performance of a liquid hydrogen tank multilayer insulation system at warm boundary temperatures of 630,530 and 152 R[C]//27th Joint Propulsion Conference. Sacramento,CA:AIAA,1991.
[14] Knoll R H,Stochl R J,Sanabria R. A review of candidate multilayer insulation systems for potential use on wet-launch LH2 tankage for the space exploration initiative Lunar missions[C]//27th Joint Propulsion Conference. Sacramento,CA:AIAA,1991.
[15] Hastings L J,Hedayat A,Brown T M. Analytical modeling and test correlation of variable density multilayer insulation for cryogenic storage[R]. USA:NASA,2004.
[16] Christie R J,Plachta D W. Zero boil-off system design and thermal analysis of the bimodal thermal nuclear rocket[J]. Space Technology&Applications International Forum-Staif,2006,813(1):494-501
[17] Haberbusch M S,Nguyen C T,Stochl R J,et al. Development of no-vent liquid hydrogen storage system for space applications[J]. Cryogenics,2010(50):541-548
[18] Plachta D W. hybrid thermal control testing of a cryogenic propellant tank[R]. USA:NASA,1999.
[19] Panzarella C H,Kassemi M. Comparison of several zero-boil-off pressure control strategies for cryogenic fluid storage in microgravity[J]. Journal of Propulsion and Power,2009,25(2):424-434
[20] Panzarella C,Plachta D,Kassemi M. Pressure control of large cryogenic tanks in microgravity[J]. Cryogenics,2004,44(6):475-483
[21] Hastings L J,Tucker S P,Flachbart R H. Marshall space flight center in-space cryogenic fluid management program overview[R]. USA:NASA,2005.
[22] Kassemi M,Panzarella C. Ventless pressure control of two-phase propellant tanks in microgravity[J]. Annals New York Academy of Sciences,2004,1027(1):511-528
[23] Segado M A,Hannon C L,Brisson J G. Collins cryocooler design for zero-boil-off storage of liquid hydrogen and oxygen in space[C]//Advances in Cryogenic Engineering:Transactions of the Cryogenic Engineering Conference-CEC. USA:American Institute of Physics,2010.
[24] Hochstein J I,Ji H C,Aydelott J C. Effect of subcooling on the on-orbit pressurization rate of cryogenic propellant tankage[C]//AIAA/ASME 4th Joint Thermophysics and Heat Transfer Conference. Boston,Massachusetts:AIAA,1986.
[25] Ryan H,Robert K,Gary O N. Thermal optimization and assessment of a long duration cryogenic propellant depot[C]//50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Nashville,Tennessee:AIAA,2012.
[26] Baik J. Zero-boil-off liquid hydrogen storage tanks[R]. USA:NASA,2009.
[27] Plachta D,Kittel P. An updated zero boil-off cryogenic propellant storage analysis applied to upper stages or depots in an LEO environment[R]. USA:AIAA,2002.
[28] Lin C S,Van Dresar N T,Hasan M M. A pressure control analysis of cryogenic storage systems[C]//AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference. Sacramento,CA:AIAA,1991.
[29] Lin C S,Van Dresar N T,Hasan M M. Pressure control analysis of cryogenic storage systems[J]. Journal of Propulsion and Power,2004,20(3):480-485
[30] Guernsey C S,Baker R S,Plachta D. Cryogenic propulsion with zero boil-off storage applied to outer planetary exploration[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Tucson,Arizona:AIAA,2005.
[31] Zakar D R,Baldauff R W,Hoang T T. Cryogenic loop heat pipe for zero-boil-off cryogen[R]. USA:AIAA,2015.
[32] Ho S H,Rahman M M. Three-dimensional analysis for liquid hydrogen in a cryogenic storage tank with heat pipe–pump system[J]. Cryogenics,2008(48):31-41
[33] Ho S H,Rahman M M. Transient analysis of cryogenic liquid-hydrogen storage tank with intermittent forced circulation[J]. Journal of Thermophysics and Heat Transfer,2010,24(2):374-380
[34] Plachta D W,Johnson W L,Feller J R. Cryogenic boil-off reduction system testing[R]. USA:AIAA,2014.
[35] Haberbusch M S,Nguyen C T,Stochl R J,et al. Development of no-vent liquid hydrogen storage system for space applications[J]. Cryogenics,2010(50):541-548
[36] Howard F,Brian L,Mark V. Liquid oxygen/liquid methane integrated propulsion system test bed[C]//47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. San Diego,California:AIAA,2011.
[37] Chato D J. Cryogenic technology development for exploration missions[C]//45th AIAA Aerospace Sciences Meeting and Exhibit Reno. Nevada:AIAA,2007.
[38] David G,Jeff S,Chris M,et al. Long term cryogenic storage technologies overview for NASA exploration applications[C]//42nd AIAA Thermophysics Conference. Honolulu,Hawaii:AIAA,2011.
[39] 冶文莲,王丽红,王田刚,等. 低温制冷机与ZBO存储系统耦合数值模拟[J]. 低温与超导,2013,41(8):19-23
Ye W L,Wang L H,Wang T G,et al. Numerical simulation of cryocooler and zero boil-off storage system coupling[J]. Cryogenics & Superconductivity,2013,41(8):19-23
[40] 冶文莲,王小军,王田刚,等. 液氢贮箱零蒸发数值模拟与分析[J]. 低温与超导,2012,40(11):11-17
Ye W L,Wang X J,Wang T G,et al. Numerical simulation and analysis of zero boil-off in a liquid hydrogen storage tank[J]. Cryogenics & Superconductivity,2012,40(11):11-17
[41] 张磊,潘雁频. 带有浸没喷射装置的液氢ZBO储箱温度场模拟研究[J]. 真空与低温,2013,19(1):19-24
Zhang L,PanY P. A numerical study on the temperature field of liquid hydrogen zero boil-off storage tank with injection nozzles[J]. Vacuum and Cryogenics,2013,19(1):19-24
[42] 程进杰,孙郁,杨建斌,等. ZBO存储低温储箱内的压力变化模拟分析[J]. 低温与超导,2014,42(1):17-20
Cheng J J,Sun Y,Yang J B,et al. Modeling the pressure variation law of cryogenic tank in the process of ZBO storage[J]. Cryogenics & Superconductivity,2014,42(1):17-20
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