先锋卫星的设计、制造和测试

R. Baumann
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引用次数: 1

摘要

1 Price, E. W.,“固体推进剂火箭发动机装药几何和弹道参数”[J] . E. T . PROPULSION, vol. 24, 1 - 2。1954,第16页。2 Vogel, J. M.,“固体推进剂火箭装药几何的准形态学方法:装药设计的家族树”,《电子推进》,第26卷,1956年2月,第102页。3 Epstein, L. I.,“圆柱形推进剂颗粒的设计”,《喷气推进》,第26卷,1956年9月,第757页。这些图表虽然不是机密的,但出现在机密报告中。可向作者索取副本。6 Wimpress, R. N.,“固体燃料火箭的内部弹道”,纽约麦格劳-希尔,1950年。7“火箭基础”,OSRD 3992。
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Design, Fabrication and Testing of the Vanguard Satellite
1 Price, E. W., "Charge Geometry and Ballistic Parameters for Solid Propellant Rocket Motor s / ' J E T PROPULSION, vol. 24, Jan.-Feb. 1954, p. 16. 2 Vogel, J. M., "A Quasi-Morphological Approach to the Geometry of Charges for Solid Propellant Rockets: The Family Tree of Charge Designs," J E T PROPULSION, vol. 26, Feb. 1956, p. 102. 3 Epstein, L. I., "The Design of Cylindrical Propellant Grains," JET PROPULSION, vol. 26, Sept. 1956, p. 757. 4, 5 These graphs, though unclassified, appear in classified reports. Copies may be obtained from the author. 6 Wimpress, R. N., "Internal Ballistics of Solid-Fuel Rockets ," McGraw-Hill, New York, 1950. 7 "Rocket Fundamentals ," OSRD 3992.
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