High accuracy stabilization system of launch vehicle with asymmetric configuration when one engine failure is possible

1998 ◽  
Vol 4 (1) ◽  
pp. 64-67 ◽  
Author(s):  
Ya.E. Aizenberg ◽  
◽  
V.A. Bataev ◽  
A.I. Kuzmin ◽  
◽  
...  
Keyword(s):  
Launch Vehicle ◽  
High Accuracy ◽  
Stabilization System ◽  
Engine Failure ◽  
Asymmetric Configuration

Molecular contamination of spacecraft surfaces in thermostatic control and orbital injection of launch vehicle nose cone

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

ESTIMATION OF AEROTHERMAL ENVIRONMENT AT THE BASE REGION OF A LAUNCH VEHICLE

2018 ◽  
Author(s):  
Jiju R. Justus ◽  
Anoop P. ◽  
Sanjoy Kumar Saha ◽  
B. Sundar
Keyword(s):  
Launch Vehicle ◽  
Base Region

REALISATION OF AN ECO-FRIENDLY SOLID PROPELLANT BASED ON HTPB -HMX-AP SYSTEM FOR LAUNCH VEHICLE APPLICATIONS

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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