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Bauman Moscow State Technical University. El № FS 77-61858. ISSN 2413-0982
Aeronautical and Rocket Space Engineering
Calculating the Insulated Car Roof Opening System Components and Strength Analysis of Car Design in Its Various Embodiments
# 02, March 2016
DOI:
10.7463/aersp.0216.0839313
V.S. Kopytov, V.M. Puchkov
pp. 1-15
Analysing a Numerical Calculation Adequacy of the Recovery Factor for Various Problem Statement Options
# 02, March 2016
DOI:
10.7463/aersp.0216.0837915
A.D. Kliukvin
pp. 16-29
Numerical Calculation of Interaction Between Plane Jet and Subsonic Flow
# 02, March 2016
DOI:
10.7463/aersp.0216.0837809
V.O. Moskalenko, I.Yu. Krasnikov
pp. 30-40
Modeling of Rocket Fuel Heating and Cooling Processes in the Interior Receptacle Space of Ground-Based Systems
# 01, January 2016
DOI:
10.7463/aersp.0116.0834621
K.I. Denisova, V.V. Chugunkov
pp. 1-13
Analysis of Approaches to the Near-Earth Orbit Cleanup from Space Debris of the Size Below10 cm
# 01, January 2016
DOI:
10.7463/aersp.0116.0833914
V.I. Maiorova, V.V. Leonov, D.A. Grishko
pp. 14-26
Temperature Condition and Spherical Shell Shape Variation of Space Gauge-Alignment Spacecraft
# 01, January 2016
DOI:
10.7463/aersp.0116.0831867
V.S. Zarubin, V.N. Zimin, G.N. Kuvyrkin
pp. 27-45
Design and Simulation of Weapon Objects
# 06, November 2015
DOI: 10.7463/aersp.0615.0827703
V.P. Strogalev, I.O. Tolkacheva, M.S. Tovarnov
pp. 1-12
Experience in Using Russian Program Complex «APM Winmachine» for Computing Local Strength of the Umbilical Mast Bearing Construction in the SR “Soyuz-2.1B"
# 06, November 2015
DOI: 10.7463/aersp.0615.0826641
V.A. Zverev, A.V. Yazykov
pp. 13-26
Modeling the Thermal Rocket Fuel Preparation Processes in the Launch Complex Fueling System
# 06, November 2015
DOI: 10.7463/aersp.0615.0826690
A.V. Zolin, V.V. Chugunkov
pp. 27-38
Approximate Method to Calculate Melting Time of Sludge-Like Cryogenic Product in Cylindrical Horizontal Tank
# 06, November 2015
DOI: 10.7463/aersp.0615.0826274
G.N. Tovarnykh
pp. 39-48
Research of Short-range Missile Motion in Terms of Different Wind Loads
# 06, November 2015
DOI: 10.7463/aersp.0615.0825096
A.N. Klishin, O.S. Shvirkina
pp. 49-66
Weight-size Optimization of Aerospace Propulsion System Heat Exchangers
# 05, September 2015
DOI: 10.7463/aersp.0515.0823574
A.D. Kliukvin, B. A. Kunikeev
pp. 1-11
Numerical Study of the Working Process in the Reducing Gas Generator of the Upper Stage Oxygen - Methane Engine
# 05, September 2015
DOI: 10.7463/aersp.0515.0821899
D.M. Yagodnikov, K.O. Chertkov, Yu.V. Antonov, Новиков А.
pp. 12-25
Optimal Control of Hypersonic Planning Maneuvers Based on Pontryagin’s Maximum Principle
# 05, September 2015
DOI: 10.7463/aersp.0515.0821077
A.Yu. Melnikov
pp. 26-37
Experimentally Studied Influence of the Bullet Head Shape on Dispersion Characteristics at Subsonic Airspeeds
# 05, September 2015
DOI: 10.7463/aersp.0515.0819074
S.N. Ilukhin, V.O. Moskalenko, A.I. Khlupnov
pp. 38-48
Local Temperature Distribution on the Spacecraft Surface under Uneven Solar Radiation
# 05, September 2015
DOI: 10.7463/aersp.0515.0820883
V.S. Zarubin, G.N. Kuvyrkin, I.Yu. Savel'eva
pp. 49-63
Project Analysis of Aerodynamics Configuration of Re-entry Сapsule-shaped Body Based on Numerical Methods for Newtonian Flow Theory
# 04, July 2015
DOI: 10.7463/aersp.0415.0813899
V.E. Minenko, D.N. Agafonov, A.G. Yakushev
pp. 1-14
Synthesis of Control Algorithm for a Leader-headed UAVs Group
# 04, July 2015
DOI: 10.7463/aersp.0415.0813298
I.O. Samodov, D.D. Dmitriev
pp. 15-24
The Multiposition Adjusting in Technological Equipment
# 04, July 2015
DOI: 10.7463/aersp.0415.0812243
B.M. Novojilov
pp. 25-36
Conversion Method of the Balance Test Results in Open Jet Tunnel on the Free Flow Conditions
# 04, July 2015
DOI: 10.7463/aersp.0415.0801630
V.T. Bui
pp. 37-50
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