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Static stability and force characteristics of a 0.02-scale model of the Saturn C-1 launch vehicle with Apollo payload for Mach number 0.31

机译：具有apollo有效载荷的土星C-1运载火箭的0.02比例模型的静态稳定性和力特性为马赫数0.31

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Frantz, G. E.;
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年度 1963
页码 1-27
总页数 27
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
APOLLO PROJECT; LAUNCH VEHICLE CONFIGURATIONS; SATURN LAUNCH VEHICLES; SPACECRAFT STABILITY; AERODYNAMIC CHARACTERISTICS; AERODYNAMIC COEFFICIENTS; STATIC STABILITY; WIND TUNNEL STABILITY TESTS;

机译：apOLLO项目;发射车辆配置; saTURN推出车辆;航天器稳定性;空气动力学特征;空气动力学系数;静态稳定性;风洞稳定性试验;

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1. Modeling of the Acoustic Response of Payload Bays Within Launch Vehicle Fairings [J] . Tyler Engberg, Umesh A. Korde Journal of Spacecraft and Rockets . 2013 ,第2期

机译：载具整流罩内有效载荷舱的声响应建模
2. Analysis of Dynamic Stability of Space Launch Vehicles under Aerodynamic Forces Using CFD Derived Data [J] . M. Trikha, S. Gopalakrishnan, D. Roy Mahapatra International Journal for Computational Methods in Engineering Science and Mechanics . 2011 ,第1a6期

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3. INFLUENCE OF THE ASYMMETRY OF CORNERING FORCES ON THE STATIC STABILITY OF A TWO-AXLE VEHICLE [J] . V. G. Verbitskii, V. A. Makarov, V. P. Sakhno International Applied Mechanics . 2004 ,第11期

机译：拐角力的不对称性对两轴车辆静态稳定性的影响
4. Measurement and Analysis of Terminal Shock Oscillation and Buffet Forcing Functions on a Launch Vehicle Payload Fairing [C] . David J. Piatak, Martin K. Sekula AIAA aviation forum . 2019

机译：运载火箭有效载荷整流罩末端冲击振荡和自助强迫功能的测量与分析
5. Aerodynamic Characteristics of a Feathered Dinosaur Measured Using Physical Models. Effects of Form on Static Stability and Control Effectiveness [O] . Dennis Evangelista, Griselda Cardona, Eric Guenther-Gleason, -1

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6. Wind Tunnel Tests and Numerical Analyses on Aerodynamic Characteristics of Epsilon Launch Vehicle at Mach 0.7 [O] . Keiichi KITAMURA, Kazuto KUZUU, Tomoko IRIKADO, 2011

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7. Static stability and force characteristics of a 0.02-scale model of the Saturn C-1 launch vehicle with Apollo payload for the Mach number range 0.70 to 3.50 [R] . Goebel, F. L. 1963

机译：具有apollo有效载荷的土星C-1运载火箭的0.02比例模型的静态稳定性和力特性，马赫数范围为0.70至3.50

Static stability and force characteristics of a 0.02-scale model of the Saturn C-1 launch vehicle with Apollo payload for Mach number 0.31

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