INTERACTIVE DESIGN AND ANALYSIS OF FUTURE LARGE SPACECRAFT CONCEPTS.

被引：0
|
作者：
Garrett, L.Bernard
机构：
来源：
NASA Technical Paper | 1981年
关键词：
Compendex;
D O I：
10.2514/6.1981-1177
中图分类号：
学科分类号：
摘要：
Spacecraft
引用
收藏
相关论文
共 50 条
  • [21] Design concepts for future large aperture wide field of view UVIS optical systems
    Woodruff, RA
    FUTURE EUV/UV AND VISIBLE SPACE ASTROPHYSICS MISSIONS AND INSTRUMENTATION, 2003, 4854 : 50 - 60
  • [22] INTERACTIVE SYSTEM FOR DESIGN OF FACTORIES OF THE FUTURE
    Furmann, Radovan
    Macus, Peter
    Stefanik, Andrej
    Hercko, Jozef
    8TH CARPATHIAN LOGISTICS CONGRESS (CLC 2018), 2019, : 116 - 122
  • [23] Design concepts for future regional aircraft
    Prestby, G
    NOUVELLE REVUE AERONAUTIQUE ASTRONAUTIQUE, 1998, (02): : 41 - 43
  • [24] Succession, development, the climax, and the complex organism: An analysis of concepts. Part I.
    Phillips, J
    JOURNAL OF ECOLOGY, 1934, 22 : 554 - 571
  • [25] Future aircraft concepts and design methods
    McDonald, Robert A.
    German, Brian J.
    Takahashi, T.
    Bil, C.
    Anemaat, W.
    Chaput, A.
    Vos, R.
    Harrison, N.
    AERONAUTICAL JOURNAL, 2022, 126 (1295): : 92 - 124
  • [26] Analysis of design development concepts for large explosion-proof motors
    Konokhov, N. N.
    ELECTRICAL ENGINEERING & ELECTROMECHANICS, 2005, (01) : 47 - +
  • [27] Interactive multimedia software design: Concepts, process, and evaluation
    Hardin, PC
    Reis, J
    HEALTH EDUCATION & BEHAVIOR, 1997, 24 (01) : 35 - 53
  • [28] The design and synthesis of a large interactive classroom
    Clouston, LL
    Kleinman, MH
    JOURNAL OF CHEMICAL EDUCATION, 1999, 76 (01) : 60 - 61
  • [29] DESIGN OF MINIMUM-MASS TRUSSES USING MATHEMATICAL PROGRAMMING METHODS INVOLVING APPROXIMATION CONCEPTS.
    Kalinin, I.N.
    Nikishin, S.S.
    Mechanics of solids, 1987, 22 (02) : 180 - 184
  • [30] NEW CONCEPTS IN DESIGN OF LARGE TRANSMITTERS
    KERNEN, H
    BROWN BOVERI REVIEW, 1970, 57 (11): : 488 - &
12345