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Levitated Launch Vehicle for Launching Satellites
International Conference Recent treads in Engineering & Technology (ICRET’2014), Feb 13-14, 2014 Batam (Indonesia)
◽
10.15242/iie.e0214525
◽
2014
◽
Keyword(s):
Launch Vehicle
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References
High accuracy stabilization system of launch vehicle with asymmetric configuration when one engine failure is possible
Kosmìčna nauka ì tehnologìâ
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10.15407/knit1998.01.064
◽
1998
◽
Vol 4
(1)
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pp. 64-67
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Cited By ~ 1
Author(s):
Ya.E. Aizenberg
◽
◽
V.A. Bataev
◽
A.I. Kuzmin
◽
◽
...
Keyword(s):
Launch Vehicle
◽
High Accuracy
◽
Stabilization System
◽
Engine Failure
◽
Asymmetric Configuration
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Molecular contamination of spacecraft surfaces in thermostatic control and orbital injection of launch vehicle nose cone
Kosmìčna nauka ì tehnologìâ
◽
10.15407/knit2007.03.003
◽
2007
◽
Vol 13
(3)
◽
pp. 3-11
Author(s):
V.A. Shuvalov
◽
◽
V.G. Tikhii
◽
L.P. Potapovych
◽
A.I. Priymak
◽
...
Keyword(s):
Launch Vehicle
◽
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
◽
10.15407/knit2019.04.022
◽
2019
◽
Vol 25
(4)
◽
pp. 22-28
Author(s):
E.H. Hladkii
◽
Keyword(s):
Launch Vehicle
◽
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
◽
10.15407/knit2019.04.003
◽
2019
◽
Vol 25
(4)
◽
pp. 3-21
Author(s):
A.V. Kondratiev
◽
◽
V.O. Kovalenko
◽
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
◽
2018
◽
Author(s):
Jiju R. Justus
◽
Anoop P.
◽
Sanjoy Kumar Saha
◽
B. Sundar
Keyword(s):
Launch Vehicle
◽
Base Region
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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
(1-6)
◽
pp. 129-134
Author(s):
Rm. Muthiah
◽
T. L. Varghese
◽
S. Somesware Rao
◽
K. N. Ninan
◽
V. N. Krishnamurthy
Keyword(s):
Solid Propellant
◽
Launch Vehicle
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FORMATION OF LAUNCH VEHICLE LOADING REGIMES FOR ADAPTATION OF TRANSPORTATION TO THE "VOSTOCHNY" COSMODROME
TsAGI Science Journal
◽
10.1615/tsagiscij.2018025299
◽
2017
◽
Vol 48
(5)
◽
pp. 469-477
Author(s):
V. A. Titov
Keyword(s):
Launch Vehicle
◽
Vehicle Loading
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AN ALGORITHMIC BASE FOR ANALYSIS OF LOADING CONDITIONS OF LAUNCH VEHICLE STRUCTURE AT MOTION IN DENSE ATMOSPHERE
TsAGI Science Journal
◽
10.1615/tsagiscij.2017022724
◽
2017
◽
Vol 48
(3)
◽
pp. 295-306
Author(s):
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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Subject Index - LAUNCH VEHICLE AND MISSILE (LV/M) TECHNOLOGY
Journal of Spacecraft and Rockets
◽
10.2514/3.57690
◽
1979
◽
Vol 16
(999)
◽
pp. 19-20
Keyword(s):
Launch Vehicle
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