scholarly journals Results of the Development of the Research Prototype of the Interactive Electronic Technical Guide for the MSV Simulator.

2021 ◽  
pp. 61-71
Author(s):  
A.I. Zhokhov

The paper considers the designation and requirement for the research prototype of the interactive electronic Technical Guide for the simulator of the Manned Space Vehicle (MSV) as well as the results of its development.

2011 ◽  
Vol 2011 ◽  
pp. 1-13 ◽  
Author(s):  
Giuseppe Pezzella ◽  
Antonio Viviani

The paper deals with the aerodynamic analysis of a manned braking system entering the Mars atmosphere with the aim to support planetary entry system design studies. The exploration vehicle is an axisymmetric blunt body close to the Apollo capsule. Several fully three-dimensional computational fluid dynamics analyses have been performed to address the capsule aerodynamic performance. To this end, a wide range of flow conditions including reacting and nonreacting flow, different angles of attack, and Mach numbers have been investigated and compared. Moreover, nonequilibrium effects on the flow field around the entry vehicle have also been investigated. Results show that real-gas effects, for all the angles of attack considered, increase both the aerodynamic drag and pitching moment whereas the lift is only slighted affected. Finally, results comparisons highlight that experimental and CFD aerodynamic findings available for the Apollo capsule in air adequately represent the static coefficients of the capsule in the Mars atmosphere.


2013 ◽  
Vol 2013 ◽  
pp. 1-9
Author(s):  
Balamati Choudhury ◽  
Hema Singh ◽  
R. M. Jha

The radio-frequency (RF) field mapping and its analysis inside a space vehicle cabin, although of immense importance, represent a complex problem due to their inherent concavity. Further hybrid surface modeling required for such concave enclosures leads to ray proliferation, thereby making the problem computationally intractable. In this paper, space vehicle is modeled as a double-curvatured general paraboloid of revolution (GPOR) frustum, whose aft section is matched to an end-capped right circular cylinder. A 3D ray-tracing package is developed which involves a uniform ray-launching scheme, an intelligent scheme for ray bunching, and an adaptive reception algorithm for obtaining ray-path details inside the concave space vehicle. Due to nonavailability of image method for concave curvatured surfaces, the proposed ray-tracing method is validated with respect to the RF field build-up inside a closed lossy cuboid using image method. The RF field build-up within the space vehicle is determined using the details of ray paths and the material parameters. The results for RF field build-up inside a metal-backed dielectric space vehicle are compared with those of highly metallic one for parallel and perpendicular polarizations. The convergence of RF field within the vehicle is analyzed with respect to the propagation time and the number of bounces a ray undergoes before reaching the receiving point.


2008 ◽  
Vol 200 (2682) ◽  
pp. 22
Author(s):  
Piers Bizony
Keyword(s):  

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