Spacecraft thermal design verification in Canada

被引:0
|
作者
Choueiry, E. [1 ]
Donato, M. [1 ]
机构
[1] David Florida Lab
来源
关键词
Canada future space program - Software package IRFLUX - Spacecraft thermal design verification - Specular baffles - Thermal balance testing - Thermal space simulation techniques;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:28 / 32
相关论文
共 50 条
  • [21] THERMAL DESIGN AND ANALYSIS OF SPACECRAFT DURING FLIGHT MISSIONS
    Farag, Ahmed M.
    Khalil, Essam E.
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2013, VOL 1, 2014,
  • [22] Dynamic space link design and verification of the spinning spacecraft mission Eu:CROPIS
    Budroweit, Jan
    Drobczyk, Martin
    2019 IEEE TOPICAL WORKSHOP ON INTERNET OF SPACE (TWIOS), 2019, : 198 - 201
  • [23] A MODULARIZED THERMAL TEST CHIP DESIGN AND VERIFICATION
    Sun, Jianjun
    Wang, Deping
    Zhou, Shiying
    Yan, Bin
    Xie, Yelei
    Pang, Jian
    Li, Guangyao
    Ouyang, Keqing
    CONFERENCE OF SCIENCE & TECHNOLOGY FOR INTEGRATED CIRCUITS, 2024 CSTIC, 2024,
  • [24] Experimental verification and comparison of different tailoring models for spacecraft electronics thermal cycling tests
    Ji, Xin-Yan
    Liu, Guo-Qing
    Wang, Jing
    Yang, Xiao-Ning
    Xiang, Shu-Hong
    Bi, Yan-Qiang
    ACTA ASTRONAUTICA, 2019, 159 : 77 - 86
  • [25] Thermal design of spacecraft solar arrays using a polyimide foam
    Bianco, N.
    Iasiello, M.
    Naso, V.
    33RD UIT (ITALIAN UNION OF THERMO-FLUID DYNAMICS) HEAT TRANSFER CONFERENCE, 2015, 655
  • [26] Stochastic spacecraft thermal design optimization with low computational cost
    Muraoka, Issamu
    Galski, Roberto L.
    de Sousa, Fabiano L.
    Ramos, Fernando M.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (06) : 1248 - 1257
  • [27] Optimizing the Intake Design of a Droplet Cooler for Thermal Regulation of Spacecraft
    Bakhvalov Y.O.
    Iosifov P.A.
    Kulikov S.N.
    Trunova E.A.
    Russian Engineering Research, 2024, 44 (02) : 177 - 179
  • [28] GRADIENT-BASED OPTIMIZATION OF SPACECRAFT AND AIRCRAFT THERMAL DESIGN
    Maciulis, Laurynas
    Belevicius, Rimantas
    AVIATION, 2020, 24 (03) : 105 - 116
  • [29] Selecting the Design Parameters of a Heat Store in Spacecraft Thermal Management
    Belyaevskii A.E.
    Sorokin A.E.
    Russian Engineering Research, 2022, 42 (12) : 1303 - 1305
  • [30] Thermophysical properties of high-thermal-conductivity graphite sheets for spacecraft thermal design
    Nagano, H
    Ohnishi, A
    Nagasaka, Y
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2001, 15 (03) : 347 - 353