Mars orbiter mission long eclipse prediction and aerobraking feasibility study

被引：0
作者：
Srivastava, Vineet K. [1 ]
Mishra, Padmdeo [1 ]
机构：
[1] ISRO Telemetry Tracking & Command Network, Flight Dynam Grp, Bangalore 560058, India
来源：
JOURNAL OF SPACE SAFETY ENGINEERING | 2023年 / 10卷 / 02期
关键词：
MOM; SPOP; STK; ODTK; Long eclipses; Aerobraking; ATMOSPHERIC MODEL; LEO;
D O I：
10.1016/j.jsse.2023.03.010
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Mars Orbiter Mission (MOM), India's first interplanetary mission, was placed in a highly elliptical orbit around the red planet Mars. In this paper, we predict Mars longer duration eclipses for the MOM space-craft using the satellite precise orbit propagator (SPOP). The longer eclipses predicted by SPOP is com-pared with the commercial propagator HPOP/STK of Ansys Inc. By considering these eclipses and based on the current fuel availability of the MOM, we have carried out the aerobraking feasibility study and the spacecraft entry on the Martian surface.(c) 2023 International Association for the Advancement of Space Safety. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：182 / 196
页数：15
相关论文
共 21 条
  • [1] [Anonymous], 1978, Spacecraft Attitude Determination and Control
  • [2] Cichocki F., Aerobraking Mission Analysis Tool for Mars Exploration Missions
  • [3] Parametric study of aerocapture for missions to Venus
    Craig, S
    Lyne, JE
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2005, 42 (06) : 1035 - 1038
  • [4] Demcak S., 2020, AIAA SCITECH FORUM
  • [5] Justh H.L., NASA/TM-2014-217499
  • [6] Mars-GRAM 2000: A Mars atmospheric model for engineering applications
    Justus, CG
    James, BF
    Bougher, SW
    Bridger, AFC
    Haberle, RM
    Murphy, JR
    Engel, S
    [J]. PLANETARY ATMOSPHERES, 2002, 29 (02): : 193 - 202
  • [7] MARS GLOBAL REFERENCE ATMOSPHERIC MODEL FOR MISSION PLANNING AND ANALYSIS
    JUSTUS, CG
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1991, 28 (02) : 216 - 221
  • [8] Long S.M., P SPACEOPS 2008 C 20
  • [9] Montenbruck O., 2012, Satellite Orbits: Models, Methods and Applications
  • [10] Prince J.L.H., 2011, AAS, P11
123