18. Development Test of Payload Fairing Separation Dynamics under Ground Conditions
Organization:
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Page: Kosm. teh. Raket. vooruž. 2017 (2); 102-106
Language: Russian
Annotation: The paper presents the original test methods with simulation of axial loads nx＜＜ 1 and nx ＞＞1 and the test stands which were used on testing the Zenit-2 ILV large-sized nose fairing.
Key words:
Bibliography:
1. Fundamentals of Spacecraft Launch Vehicles Designing / Under the editorship of V. P. Mishin. М., 1991. 415 p.
2. Kolesnikov K. S., Kozlov V. V., Kokushkin V. V. Flying Vehicles Stages Separation Dynamics. М., 1977. 224 p.
3. Аuthor’s Certificate 285792. Stand for Testing Rocket Fairing Separation in Ground Conditions / O. A. Semenenko, E. I. Shevtsov, V. A. Gontarovsky, V. A. Petrushevsky et al. Claimed 10.05.1989.
4. Аuthor’s Certificate 323879. Method of g-Loads Simulation during Testing of Separation Systems of Cylindrical-Conical Fairing that Separates into Doors / E. I. Shevtsov, V. A. Gontarovsky et al. Claimed 07.02.1989.
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