SPACECRAFT STRUCTURE AND THERMAL DESIGN CONSIDERATIONS

被引：7

作者：

HRYCAK, P

KOONTZ, DE

WITTENBERG, AM

MAGGS, C

STAFFORD, JW

UNGER, BA

机构：

来源：

BELL SYSTEM TECHNICAL JOURNAL | 1963年 / 42卷 / 02期

关键词：

D O I：

10.1002/j.1538-7305.1963.tb04025.x

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

引用

页码：973 / +

页数：1

共 13 条

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[3] SPACECRAFT TEST AND EVALUATION PROGRAM [J].

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JONASSON, GC ;

SWIFT, RA .

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[4]

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[5] THERMAL CONTROL OF THE EXPLORER SATELLITES [J].

HELLER, G .

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[6] TEMPERATURE DISTRIBUTION IN A SPINNING SPHERICAL SPACE VEHICLE [J].

HRYCAK, P .

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[7]

HRYCAK P, 1962, ARSJ-AM ROCKET SOC J, V32, P1294

[8]

HRYCAK P, 1963, P I ENVIRONMENTAL SC, P477

[9]

HRYCAK P, TO BE PUBLISHED

[10]

HUTCHISON PT, 1963, BELL SYST T, V42

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