Methodological aspects for designing a launch vehicle through the efficiency criterion

1Mashchenko, AN, 2Fediakin, AI
1Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
2Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and State Space Agency of Ukraine, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2004, 10 ;(2-3):068-073
Publication Language: Russian
Models for the determination of the technical and economical characteristics of systems of commercial launch vehicles through the net income criterion are proposed. Reliability is used as a parameter relating the income and cost with technical characteristics. The possibility to validate the launch cost with allowance made for competitiveness is examined. It is assessed taking into account priorities of a decision-making person.
Keywords: commercial launch vehicles, efficiency criterion, social sciences
1. Volkov E. B., Dvorkin V. Z., Prokudin A. I., Shishkin U. N. Technical Features of the Missile System Effectiveness,256 p. (Mashinostroenie Publ., Moscow, 1989) [In Russian].
2. Germeier Yu. B. Introduction to Operations Research Theory, 384 p. (Nauka, Moscow, 1975) [In Russian].
3. Drakin I. I. Basics of designing unmanned aerial vehicles, taking into account economic efficiency, 224 p. (Mashinostoroenie, Moscow, 1973) [In Russian].
4. Kelle D. E. Models of cost in the rocket and space technology [Modeli stoimosti v raketno-kosmicheskoj tehnike]. Voprosy raketnoj tehniki, No. 12, 3—63 (1972) [In Russian].
5. Kononenko I. The method of rapid analysis of the competitiveness of products. Jekonomika Ukrainy, No. 2, 80—83 (1998) [In Russian].
6. Konyukhov S. N., Fedyakin A. I. Probability-statistical methods to design space launch systems, 250p. (Ukraine’s National Academy of Sciences and National Space Agency’s Institute of Engineering Mechanics, Dnepropetrovsk, 1997) [In Russian].
7. Larichev O. I., Petrovsky A. B. Decision support systems for semistructured problems: Requirements and Limitations [Sistemy   podderzhki prinjatija reshenij dlja slabostrukturirovannyh problem: Trebovanija i ogranichenija]. In: Cheloveko-mashinnye procedury prinjatija reshenij: Sb. tr., 4—13. (VNIISI, Moscow, 1988) [In Russian].
8. Matveevskii S. F. Fundamentals of the systems design of aircraft, 240 p. (Izdatel'stvo Mashinostroenie, Moscow, 1987) [In Russian].
9. Mashhenko A. N., Fedjakin A. I. The main stages of the design of carrier rockets on economic criteria [Osnovnye jetapy proektirovanija raket-nositelej po jekonomicheskomu kriteriju]. Tekhicheskaya Mekhanika, Is. 2, 134—138 (2001) [in Russian].
10. Mishin V. P. Fundamentals of aerial vehicles (transport systems) [Osnovy proektirovanija letatel'nyh apparatov (transportnye sistemy)], 360 p. (Mashinostroenie, Moscow, 1985) [In Russian].
11. Müller P. H., Neumann P., Storm R. Tafeln der mathematischen Statistik, 278 p. (Finansy i statistika, Moscow, 1982) [In Russian].
12. Nikolaev V. I., Bruk V. M. Systems Engineering: Methods and Applications, 199 p. (Mashinostroenie, Leningrad, 1985) [In Russian].
13. Rash B. S., Brjeken D., Makkormik G. P. Optimization of design parameters of carrier rockets on the criterion of minimum cost [Optimizacija proektnyh parametrov raket-nositelej po kriteriju minimal'noj stoimosti]. Voprosy raketnoj tehniki, No. 2, 16—29 (1968) [In Russian].
14. Sarkisyan S. A., Minaev É. S. Economic Evaluation of Aircraft, 180 p. (Mashinostroenie, Moscow, 1972) [in Russian].
15. Sinyukov A. M., Volkov L. I., Lvov A. I., Shishkevich A. M. Ballistic Solid-Propellant Rockets, 512 p. (Voenizdat, Moscow, 1972) [in Russian].
16. Taha H. A. Operations Research: An Introduction, 496 p. (Mir, Moscow, 1985) [in Russian].

17. Faskhiev Kh. A. Evaluation of competitiveness of new technology [Ocenka konkurentosposobnosti novoj tehniki]. Marketing, No. 6, 25—35 (1998) [in Russian].