AN ALGORITHMIC BASE FOR ANALYSIS OF LOADING CONDITIONS OF LAUNCH VEHICLE STRUCTURE AT MOTION IN DENSE ATMOSPHERE

2017 ◽  
Vol 48 (3) ◽  
pp. 295-306
Author(s):  
V. A. Titov
Keyword(s):  
Launch Vehicle ◽  
Loading Conditions ◽  
Vehicle Structure ◽  
Dense Atmosphere

The Displacement Measurement of Ground Wind Loads for Launch Vehicle

2014 ◽  
Vol 568-570 ◽  
pp. 100-105
Author(s):  
Tao Wang ◽  
Ze Huan Huang ◽  
Hui Zhang ◽  
Bin Zheng
Keyword(s):  
Image Processing ◽  
Digital Image Processing ◽  
Pressure Measurement ◽  
Measurement Model ◽  
Launch Vehicle ◽  
Displacement Measurement ◽  
Wind Pressure ◽  
Wind Loads ◽  
Structure Model ◽  
Vehicle Structure

This paper presented a method of the displacement measurement of ground wind loads for launch vehicle based on laser and Digital Image Processing Technology. The launch vehicle structure model was built by calculating the wind pressure. Measurement model and algorithm for single laser were given. In view of nonrigid component, a method for computing the centroid displacement was presented. Error analysis and error reducing measures were preliminarily discussed.

VERIFICATION OF A COMPUTATIONAL DYNAMIC MODEL OF A LAUNCH VEHICLE STRUCTURE

2018 ◽  
Vol 49 (1) ◽  
pp. 93-103
Author(s):  
Aleksandr Georgievich Bakhtin ◽  
Vasilii Aleksandrovich Titov
Keyword(s):  
Dynamic Model ◽  
Launch Vehicle ◽  
Vehicle Structure

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
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