Feasibility of the recent Russian nuclear electric propulsion concept: 2010

被引:8
|
作者
Zakirov, Vadim [1 ]
Pavshook, Vladimir [2 ]
机构
[1] Tsinghua Univ, Sch Aerosp, Beijing 100084, Peoples R China
[2] Russian Res Ctr Kurchatov Inst, Moscow 123182, Russia
关键词
D O I
10.1016/j.nucengdes.2011.02.010
中图分类号
TL [原子能技术]; O571 [原子核物理学];
学科分类号
0827 ; 082701 ;
摘要
The paper introduces recent Russian nuclear electric propulsion (NEP) concept for space exploration. The concept advantages are listed along with future missions. The current development status for the two main enabling technologies is presented and the feasibility analysis of the up-to-date experience is performed. The main features of NEP concept are discussed. Revision of these features and available technologies demonstrates that the NEP concept is a logical continuation of the previous efforts by the former Soviet Union. Because no breakthrough technologies are needed for NEP development while the existing technologies only need to be adapted to the megawatt (MW) class NEP the development is considered technically feasible, low risk program likely to succeed unless cancelled by the listed non-technical reasons. Successful NEP space vehicle development is going to bring practical space exploration of solar system to the new level as well as require supplementary payload program, supporting monitoring and communication radar networks. Nuclear safety during future NEP missions can be ensured by adherence to the United Nations guidelines in the same way it was done during the Soviet Topaz Nuclear Power System (NPS) missions. (C) 2011 Elsevier B.V. All rights reserved.
引用
收藏
页码:1529 / 1537
页数:9
相关论文
共 50 条
  • [1] Recent advances in nuclear powered electric propulsion for space exploration
    Cassady, R. Joseph
    Frisbee, Robert H.
    Gilland, James H.
    Houts, Michael G.
    LaPointe, Michael R.
    Maresse-Reading, Colleen M.
    Oleson, Steven R.
    Polk, James E.
    Russell, Derrek
    Sengupta, Anita
    ENERGY CONVERSION AND MANAGEMENT, 2008, 49 (03) : 412 - 435
  • [2] A realistic concept of a manned Mars mission with nuclear-electric propulsion
    Loeb, H. W.
    Petukhov, V. G.
    Popov, G. A.
    Mogulkin, A. I.
    ACTA ASTRONAUTICA, 2015, 116 : 299 - 306
  • [3] AZIPOD - A BOLD ELECTRIC PROPULSION CONCEPT
    不详
    NAVAL ARCHITECT, 1994, : E132 - E132
  • [4] Nuclear modules for space electric propulsion
    Difilippo, FC
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 1998, PTS 1-3: 1ST CONF ON GLOBAL VIRTUAL PRESENCE; 1ST CONF ON ORBITAL TRANSFER VEHICLES; 2ND CONF ON APPLICAT OF THERMOPHYS IN MICROGRAV; 3RD CONF ON COMMERCIAL DEV OF SPACE; 3RD CONF ON NEXT GENERAT LAUNCH SYST; 15TH SYMP ON SPACE NUCL POWER AND PROPULSION, 1998, (420): : 1281 - 1287
  • [5] On the Feasibility of a LiS Battery for Aircraft Electric Propulsion
    Hess, Robert
    Arbogast, Robert
    Parke, Caitlin
    Subramaniam, Akshay
    Kolluri, Suryanarayana
    Subramanian, Venkat
    2019 AIAA/IEEE ELECTRIC AIRCRAFT TECHNOLOGIES SYMPOSIUM (EATS), 2019,
  • [6] NUCLEAR ELECTRIC PROPULSION MISSIONS.
    Jones, R.M.
    Sauer, C.G.
    JBIS. Journal of the British Interplanetary Society, 1984, 37 (08): : 395 - 400
  • [7] Feasibility Analysis of Integration of Electric Propulsion Technology and Traditional Propulsion Technology
    Zhang, Shaowei
    Wang, Wenzhang
    2021 12TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE), 2021, : 12 - 16
  • [8] NUCLEAR-ELECTRIC PROPULSION - MANNED MARS PROPULSION OPTIONS
    PALASZEWSKI, B
    BROPHY, J
    KING, D
    CASE FOR MARS 111 : STRATEGIES FOR EXPLORATION - TECHNICAL, 1989, 75 : 431 - 451
  • [9] A Closed Brayton power conversion unit concept for nuclear Electric Propulsion for deep space missions
    Toyner, CR
    Fowler, B
    Matthews, J
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - STAIF 2003, 2003, 654 : 677 - 684
  • [10] Russian nuclear forces, 2010
    Norris, Robert S.
    Kristensen, Hans M.
    BULLETIN OF THE ATOMIC SCIENTISTS, 2010, 66 (01) : 74 - 81