Methods to Reduce Material Intensity of Tail Sections of Launch Vehicles

Author:

Dehtiarov Maksym O., ,Dziuba Anatolii P.,Avramov Kostiantyn V.ORCID,Sirenko Volodymyr M., , ,

Publisher

National Academy of Sciences of Ukraine (Co. LTD Ukrinformnauka)

Reference19 articles.

1. 1. Degtyarev, A. V. (2014). Raketnaya tekhnika. Problemy i perspektivy [Rocket technology. Problems and prospects]: Selected scientific and technical publications. Dnepropetrovsk: ART-PRESS, 420 p.

2. 2. Mossakovskiy, V. I., Makarenkov, A. G., Nikitin, P. I., Savin, Yu. I., & Spiridonov, I. N. (1990). Prochnost raketnykh konstruktsiy [Strength of rocket structures]. Moscow: Vysshaya shkola, 358 p.

3. 3. Balabukh, L. I., Kolesnikov, K. S., Zarubin, V. S., Alfutov, N. A., Usyukin, V. I., & Chizhov, V. F. (1969). Osnovy stroitelnoy mekhaniki raket [Fundamentals of structural mechanics of rockets]. Moscow: Vysshaya shkola, 496 p.

4. 4. Usyukin, V. I. (1988). Stroitelnaya mekhanika konstruktsiy kosmicheskoy tekhniki [Structural mechanics of structures of space technology]. Moscow: Mashinostroyeniye, 392 p.

5. 5. Kurenkov, V. I. & Yumashev, L. P. (2005). Vybor osnovnykh proyektnykh kharakteristiki konstruktivnogo oblika raket nositeley [Choice of the main design characteristics of the design of the carrier rockets]. Samara: Samara Aerospace University, 240 p.

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