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Space shuttle: Aerodynamic characteristics of various MDAC space shuttle ascent configurations with parallel burn pressure-fed and SRM boosters. Volume 3: Tank T4 configurations

机译：航天飞机：各种mDaC航天飞机上升配置的空气动力学特性，带有平行燃烧压力馈电和sRm增压器。第3卷：坦克T4配置

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作者
Jarrett, T. W.;
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年度 1972
页码 1-835
总页数 835
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; SPACE SHUTTLES; SPACECRAFT COMPONENTS; SPACECRAFT CONFIGURATIONS; ASCENT TRAJECTORIES; FUEL TANKS; SUPERSONIC SPEED; WIND TUNNEL MODELS;

机译：空气动力学特征;太空沙滩;航天器组件;航天器配置; asCENT TRaJECTORIEs;汽油桶;超音速;风洞模型;

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专利

1. LMSC/NRC Unsteady Aerodynamics Program to Ensure the Structural Integrity of the Space Shuttle Launch Configuration [J] . Lars E. Eriscss, Martin E. Beyers Canadian Aeronautics and Space Journal . 2001,第3期

机译：LMSC / NRC不稳定空气动力学计划，以确保航天飞机发射构型的结构完整性
2. LMSC/NRC Unsteady Aerodynamics Program to Ensure the Structural Integrity of the Space Shuttle Launch Configuration [J] . Lars E. Eriscss, Martin E. Beyers Canadian Aeronautics and Space Journal . 2001,第3期

机译：LMSC / NRC不稳定空气动力学计划，以确保航天飞机发射构型的结构完整性
3. Dynamical Analysis and Synthesis of Inertia-Mass Configurations of a Spacecraft with Variable Volumes of Liquids in Jet Engine Tanks [J] . ANTON V. DOROSHIN, MIKHAIL M. KRIKUNOV WSEAS Transactions on Systems . 2014,第Pta2期

机译：喷气发动机油箱中液体体积可变的航天器惯性质量构型的动力学分析和综合
4. Preliminary Analysis of Ascent Loads on a Space Shuttle Liquid Flyback Booster Configuration [C] . Reynaldo J. Gomez, Jeffrey P. Slotnick AIAA applied aerodynamics conference . 1995

机译：航天飞机液体反激助力器配置中上升载荷的初步分析
5. Flame-spreading phenomena in a head-end fin-slot segment of a subscale motor simulating the space shuttle boosters. [D] . Moore, Jeffrey D. 2008

机译：模拟航天飞机助推器的小规模电动机的首尾鳍槽段中的火焰蔓延现象。
6. Flow-field measurements in the windward surface shock layer of space shuttle orbiter configurations at Mach number 8 [O] . Carter, L. D., Martindale, W. R. 1975

机译：马赫数为8的航天飞机轨道飞行器构型的迎风面激波层中的流场测量
7. Space Shuttle Aerodynamic Characteristics of Various MDAC Space Shuttle Ascent Configurations with Parallel Burn Pressure-Fed and Srm Boosters. Volume 3 Tank T4 Configurations [R] . Jarrett, T. W. 1972

机译：具有平行燃烧压力和srm增压器的各种mDaC航天飞机上升配置的航天飞机气动特性。第3卷Tank T4配置

Space shuttle: Aerodynamic characteristics of various MDAC space shuttle ascent configurations with parallel burn pressure-fed and SRM boosters. Volume 3: Tank T4 configurations

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