Effiecency criterion for selection of design parameters of aerospace system
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| 1Kalynychenko, DS, 2Baranov, Ye.Yu., 2Poluian, MV 1Yuzhnoye State Design Office, Dnipro, Ukraine 2Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine |
| Space Sci.&Technol. 2016, 22 ;(2):48-51 |
| https://doi.org/10.15407/knit2016.02.048 |
| Publication Language: Ukrainian |
Abstract: We describe method of selection of design parameters for aerospace system, appointed for delivery of micro-satellites to Low-Earth Orbit. The method is developed for the analysis of existing launch vehicles, forming the base design parameters, performance criteria and determination of rational design parameters of aerospace system.
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| Keywords: aerospace system, design parameters |
References:
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2. Kalynychenko D. S., Kashanov A. E., Baranov E. Yu., et al. The choice of design parameters of aerospace systems. Kosmich. tehn. Raketnoe vooruzhenie, N 1, 80—88 (2014) [in Russian].
3. Kobelev V. N., Milovanov A. G. Launch vehicles of spacecrafts, 520 p. (Restart, Moscow, 2009) [in Russian].
4. Lukashevich V. P., Afanas'ev I. B. Kosmicheskie kryl'ja, 496 p. (LenTa Stranstvij, Moscow, 2009) [in Russian].
5. Mishin V. P., Bezverbyj V. K., Pankratov B. M., et al. Fundamentals of aircrafts design (Transportation Systems): Textbook for technical universities. 360 p. (Mashinostroenie, Moscow, 1985) [in Russian].
6. David A. Young Responsive Access Small Cargo Affordable Launch (RASCAL) independent performance evaluation. AE8900 Special Project Report. Atlanta, Georgia 30332- 0150, May, 2004. (Atlanta, 2004).
7. Pegasus User’s Guide. Release 5.0., 103 p. (Orbital Sciences Corporation, 2000).