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THE FLIGHT PHASES, FACTORS AND LOADS ACTING ON THE SPACECRAFT DURING THE PLANETS SCIENTIFIC MISSIONS USING THE HYDROGEN-OXYGEN PROPELLANT
https://doi.org/10.15518/isjaee.2016.09-10.095-106
Abstract
The paper deals with the main flight phases of the spacecraft rockets and automatic spacecrafts for the planets scientific missions including the active flight with firing engines in the Earth atmosphere; the flight on the LEO; transfer flight to the other planets; entry to the planet atmosphere; flight with the parachute system; landing and operation on the planet surface.
The schemes of the spacecraft landing to the surfaces of the Venus, the Mars, the Moon the Earth satellite are presented. Main systems of descend and landing spacecraft main systems are also presented.
The paper describes the main natural and artificial factors and loadings, acting during the spacecraft operation, the vibration and acoustic loads; linear accelerations, natural and the Earth’s artificial electromagnetic belts, galactic and solar space radiation, the solar heat radiations, meteorites, space vacuum, electromagnetic radiation, low gravity, space waste, aerial gaseous and dynamic factors.
The theoretical and experimental study of the space environment and loadings acting on the automated spacecraft during its operational phases should be performed at the phase of experimental development to provide the specified reliability.
A reasonability of the lunar surface base creation has been substantiated. The base will be provided with the systems of hydrogen and oxygen production. Here the automated spacecraft propulsion system will be refilled with the propellant components. After that the spacecraft can fly to the deep space objects.
About the Authors
A. G. Galeyev
Science and Testing Center of the Rocket-Space Industry
Russian Federation
Russian Federation
9 Babushkin str., Peresvet, Moscow Region, 141320
Information about the author: D.Sc. (engineering), professor, Laureate of USSR Council of Ministers in the field of science and technology, member of the RACTs, Chief Researcher of the PCF “SIC RSI”, professor of “Management of operation of RSS” of Moscow Aviation Institute (National Research University); scientific and pedagogical experience is of 43 years. Participated in working out a number of systems for missile and space programs «Space-1», «Space-3», «N1L3», «EnergiaBuran», «GSLV», «Angara» and others.
Education: Kazan Aviation Institute, 1961.
Research area: theory and practice ground tests of rocket engines and movingenforcement units; hydro and gas dynamics processes in power plants; research in the field of hydrogen technology.
Publications: more than 200, including 7 monographs, 6 textbooks, 44 patents for inventions.
Y. V. Zakharov
Moscow State University of the Information Technologies, Radiotechnique and Electronics
Russian Federation
Russian Federation
78 Vernadsky str., Moscow, 119454
Information about the author: D.Sc. (engineering), professor of the “Applied Synergy” department of the Moscow State University of Information technologies; scientific and pedagogical experience is more than 40 years; participated in working out a number of systems for missile and space programs including the “Luna-4”, …, “Luna-24”, “Lunokod-1”, “Mars-6,7”, “Venera-15, 16”, “VEGA-1,2”; a member of liquidation of the Chernobyl disaster consequences.
Education: Moscow Aviation Institute.
Research area: experimental development of the complex technical systems; operational management of the rockets and spacecrafts.
Publications: more than 150, including 2 monographs, 4 handbooks, 1 textbooks, 14 patents for inventions.
N. A. Markachev
Lavochkin Association (Science and Production Association“NPO im. S.A. Lavochkina”)
Russian Federation
Russian Federation
24 Leningradskaya str., Khimki, Moscow Region, 141400
Information about the author: Ph.D. (engineering), laureate of Russian Federation Government Prize in the scientific area; correspondent member of the Russian Academy of the Cosmonautics by K.E. Tsiolkovsky, Director – Chief Expert of the “VEGA” International Project on the propellant tanks. More than 50 years he had taken part in the Lavochkin Association space activities as a chief of the materials science division.
Education: Moscow Aviation Technology Institute.
Research area: materials science in the rockets and space technology; ground experimental development the automatic spacecrafts.
Publications: more than 150, including 50 articles, 5 monographies, 30 inventions, 2 patents.
D. N. Mikhaylov
Lavochkin Association (Science and Production Association“NPO im. S.A. Lavochkina”)
Russian Federation
Russian Federation
24 Leningradskaya str., Khimki, Moscow Region, 141400
Information of the author: General Designer Deputy on the testing of the Lavochkin Association; participated in the design and development of the following spacecrafts: “Electro-L”, “SpektrR”, “Luna-Glob”, “Spekt-RG”, “MKAFKI” and underes.
Education: Moscow Aviation Institute.
Research area: the automatic spacecrafts design and ground development.
Publications: more than 50.
References
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Review
For citations:
Galeyev A.G., Zakharov Y.V., Markachev N.A., Mikhaylov D.N. THE FLIGHT PHASES, FACTORS AND LOADS ACTING ON THE SPACECRAFT DURING THE PLANETS SCIENTIFIC MISSIONS USING THE HYDROGEN-OXYGEN PROPELLANT. Alternative Energy and Ecology (ISJAEE). 2016;(9-10):95-106. (In Russ.) https://doi.org/10.15518/isjaee.2016.09-10.095-106
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