Development of a method for extracting a guaranteed fuel supply in the tanks of the spent stage of launch vehicles

Authors

  • А.М. Bapyshev Al-Farabi Kazakh National University, 71 al-Farabi ave., Almaty, Kazakhstan; Almaty University of Energy and Communications named after G.Daukeeva, 126/1 Baitursynov st., Almaty, Kazakhstan
  • Г.Т. Ермолдина Казахский национальный университет имени аль-Фараби, пр. аль-Фараби, 71, Алматы, Казахстан; Институт информационных и вычислительных технологий, ул. Курмангазы, 29, Алматы, Казахстан
  • V.I. Тrushlyakov Omsk State Technical University, 11 Mira ave., Omsk, Russia
  • A.U. Utegenova Institute of Information and Computing Technologies, 29 Kurmangazy st., Almaty, Kazakhstan; Almaty University of Energy and Communications named after G.Daukeeva, 126/1 Baitursynov st., Almaty, Kazakhstan
  • К.M. Myrzabekov Almaty University of Energy and Communications named after G.Daukeeva, 126/1 Baitursynov st., Almaty, Kazakhstan
  • К.Zh. Аbildayeva Branch VOSKHOD MAI, 5 Gagarina str., Baikonur, Kazakhstan

DOI:

https://doi.org/10.18321/cpc538

Keywords:

газификация, отработавшая ступень, теплоноситель, гарантийный запас топлива, ракета-носитель.

Abstract

Remains of guaranteed fuel represent the additional stocks of propellant components in the rocket blocks of the stage of launch vehicles (ILV), designed to compensate for the disturbing factors acting in flight on the LV, and are characterized by carcinogenic and mutagenic effects on the environment. To solve the problem of reducing the technogenic load, a method is proposed for extracting a guaranteed reserve of fuel in the tanks of the worked off stage of launch vehicle. The method is based on the generation of heat due to the combustion of liquefied propane and oxygen vapor directly in fuel tanks. The amount of heat is determined from the condition of evaporation of liquid residues of oxygen and kerosene. The authors have developed a method for extracting the guaranteed fuel reserve in the tanks of the worked off stage in full. The proposed method will make it possible to use the remaining fuel for the controlled descent of the worked off stage.

References

(1). Lesnyak IYu, Dron MM, Zharikov KI, Lavruk SA (2016) In the world scientific discoveries [V mire nauchnyh otkrytij] 12.1(72):369-379. (In Russian)

(2). Suimenbayev BT, Trushlyakov VI, Yermoldina GT, Suimenbayeva ZhB, Bapyshev AM (2019) News of The National Academy of Sciences of The Republic of Kazakhstan. Physico-Mathematical Series [Izvestiya Nacional’noj akademii nauk Respubliki Kazahstan. Fizikomatematicheskaya seriya] 1(323):5-13. (in Russian). https://doi.org/10.32014/2019.2518-1726.1

(3). Zharikov KI (2014) Dynamics of systems, mechanisms and machines [Dinamika sistem, mekhanizmov i mashin] 2:224-227. (In Russian)

(4). Belkova ME (2014) Investigation of gas generating mixtures for gasification of rocket fuel residues in rocket stage tanks. Proceedings of XXXVIII acad. astronaut readings; under total ed. A.K. Medvedeva, Omsk, Russia. P.1-13. (In Russian)

(5). Urban VA (2018) Development of an onboard system for the evaporation of unusable fuel residues in launch vehicle tanks [Razrabotka bortovoj sistemy ispareniya nevyrabatyvaemyh ostatkov topliva v bakah raket-nositelej] Proceedings of the XII All-Russian Scientific Conference «Problems of development, manufacture and operation of rocket and space technology and training of engineering personnel for the aerospace industry», dedicated to the memory of the chief designer of the Polet software A.S. Klinyshkova, Omsk, Russia. P.116-122. (in Russian)

(6). Belkova ME (2014) Development of an onboard system for the evaporation of unusable fuel residues in the tanks of launch vehicles. Proceedings of the XII All-Russian scientific conference «Problems of development, manufacture and operation of rocket and space technology and training of engineering personnel for the aerospace industry», dedicated to the memory of the chief designer of the Polet software A.S. Klinyshkov, Omsk, Russia. P.116-122 (In Russian)

(7). Titov BA, Rychkov SA (2007) Vestnik SNAU [Vestnik SGAU] 1:90-97. (In Russian)

(8). Kuznetsov YuL, Ukraintsev DS (2016) Aircraft and Space Rocket Engineering 15(1):73-80. (in Russian). https://doi.org/10.18287/2412-7329-2016-15-1-73-80

Published

2022-03-16

How to Cite

Bapyshev А., Ермолдина, Г., Тrushlyakov V., Utegenova, A., Myrzabekov К., & Аbildayeva К. (2022). Development of a method for extracting a guaranteed fuel supply in the tanks of the spent stage of launch vehicles. Combustion and Plasma Chemistry, 20(2), 143–148. https://doi.org/10.18321/cpc538

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