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Ariane Launch Vehicle: A European Program
Satellite Communications: Future Systems
◽
10.2514/5.9781600865282.0377.0388
◽
1977
◽
pp. 377-388
Keyword(s):
Launch Vehicle
◽
European Program
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Keyword(s):
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High accuracy stabilization system of launch vehicle with asymmetric configuration when one engine failure is possible
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1998
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Stabilization System
◽
Engine Failure
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Asymmetric Configuration
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Molecular contamination of spacecraft surfaces in thermostatic control and orbital injection of launch vehicle nose cone
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10.15407/knit2007.03.003
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Keyword(s):
Launch Vehicle
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Thermostatic Control
◽
Nose Cone
◽
Orbital Injection
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Evaluation of hazard for linear objects in case of launch vehicle failure in flight phase
Kosmìčna nauka ì tehnologìâ
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10.15407/knit2019.04.022
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pp. 22-28
Author(s):
E.H. Hladkii
◽
Keyword(s):
Launch Vehicle
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Flight Phase
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Optimization of design parameters of the main composite fairing of the launch vehicle under simultaneous force and thermal loading
Kosmìčna nauka ì tehnologìâ
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10.15407/knit2019.04.003
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2019
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Vol 25
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pp. 3-21
Author(s):
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◽
◽
V.O. Kovalenko
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Keyword(s):
Thermal Loading
◽
Launch Vehicle
◽
Design Parameters
◽
Optimization Of Design Parameters
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ESTIMATION OF AEROTHERMAL ENVIRONMENT AT THE BASE REGION OF A LAUNCH VEHICLE
10.1615/ihmtc-2017.1460
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2018
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Author(s):
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Launch Vehicle
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REALISATION OF AN ECO-FRIENDLY SOLID PROPELLANT BASED ON HTPB -HMX-AP SYSTEM FOR LAUNCH VEHICLE APPLICATIONS
International Journal of Energetic Materials and Chemical Propulsion
◽
10.1615/intjenergeticmaterialschemprop.v4.i1-6.150
◽
1997
◽
Vol 4
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pp. 129-134
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Rm. Muthiah
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T. L. Varghese
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S. Somesware Rao
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K. N. Ninan
◽
V. N. Krishnamurthy
Keyword(s):
Solid Propellant
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Launch Vehicle
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FORMATION OF LAUNCH VEHICLE LOADING REGIMES FOR ADAPTATION OF TRANSPORTATION TO THE "VOSTOCHNY" COSMODROME
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10.1615/tsagiscij.2018025299
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Author(s):
V. A. Titov
Keyword(s):
Launch Vehicle
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AN ALGORITHMIC BASE FOR ANALYSIS OF LOADING CONDITIONS OF LAUNCH VEHICLE STRUCTURE AT MOTION IN DENSE ATMOSPHERE
TsAGI Science Journal
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10.1615/tsagiscij.2017022724
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2017
◽
Vol 48
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◽
pp. 295-306
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V. A. Titov
Keyword(s):
Launch Vehicle
◽
Loading Conditions
◽
Vehicle Structure
◽
Dense Atmosphere
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Ascent Guidance for Launch Vehicle Based on Receding Horizon Control
2020 39th Chinese Control Conference (CCC)
◽
10.23919/ccc50068.2020.9188647
◽
2020
◽
Author(s):
Qianwei He
◽
Ye Yang
◽
Lei Liu
◽
Zhongtao Cheng
Keyword(s):
Launch Vehicle
◽
Receding Horizon Control
◽
Receding Horizon
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