scholarly journals Study of power-to-weight ratio of the electrothermal propulsion system of nanosatellite maneuvering satellite platform

2018 ◽  
Vol 944 ◽  
pp. 012020 ◽  
Author(s):  
V N Blinov ◽  
I S Vavilov ◽  
V V Kositsin ◽  
A I Lukyanchik ◽  
V I Ruban ◽  
...  
2017 ◽  
Vol 5 (2) ◽  
pp. 004-016
Author(s):  
V. N. Blinov ◽  
◽  
I. S. Vavilov ◽  
V. V. Kositsin ◽  
A. I. Lukyanchik ◽  
...  

2022 ◽  
pp. 1-38
Author(s):  
Qi Zhang ◽  
Yizhong Wu ◽  
Li Lu ◽  
Ping Qiao

Abstract High dimensional model representation (HDMR), decomposing the high-dimensional problem into summands of different order component terms, has been widely researched to work out the dilemma of “curse-of-dimensionality” when using surrogate techniques to approximate high-dimensional problems in engineering design. However, the available one-metamodel-based HDMRs usually encounter the predicament of prediction uncertainty, while current multi-metamodels-based HDMRs cannot provide simple explicit expressions for black-box problems, and have high computational complexity in terms of constructing the model by the explored points and predicting the responses of unobserved locations. Therefore, aimed at such problems, a new stand-alone HDMR metamodeling technique, termed as Dendrite-HDMR, is proposed in this study based on the hierarchical Cut-HDMR and the white-box machine learning algorithm, Dendrite Net. The proposed Dendrite-HDMR not only provides succinct and explicit expressions in the form of Taylor expansion, but also has relatively higher accuracy and stronger stability for most mathematical functions than other classical HDMRs with the assistance of the proposed adaptive sampling strategy, named KKMC, in which k-means clustering algorithm, k-Nearest Neighbor classification algorithm and the maximum curvature information of the provided expression are utilized to sample new points to refine the model. Finally, the Dendrite-HDMR technique is applied to solve the design optimization problem of the solid launch vehicle propulsion system with the purpose of improving the impulse-weight ratio, which represents the design level of the propulsion system.


Author(s):  
Lester B. Veno

The various design parameters which affect the performance versus speed of the compound helicopter are studied, such as disk loading, solidity, and tip speed schedule. Additional variables which are part of the compound design, such as propeller diameter, wing lift, and equivalent drag, are similarly studied. The interrelationship of each parameter is shown in terms of the total lift/propulsive power required. The study further presumes a fixed mission requirement against which each parameter is evaluated and optimized based on proper sizing and fuel usage. The study includes the direct effect of engine power/weight ratio and SFC. The paper lays a foundation for future performance analyses of this hybrid vehicle.


Author(s):  
V. N. Blinov ◽  
◽  
V. V. Kositsin ◽  
A. I. Lukyanchik ◽  
P. V. Stepen ◽  
...  

In the paper have been discussed nanosetellite propulsion system normalization actual themes, as well their acknowledgement by the testing results. To secure needed survival probability P≥0,995, the propulsion system bottlenecks normalized values are defined. The results of propulsion system fatigue test and reliability evaluation also have been presented. The realized count of propulsion system pulse mode switching is 15700. The actual value testing propulsion system survival probability is P=0,9979. That confirms the ability of nanosatellite propulsion system demanded reliability.


Author(s):  
Chris M. Waldhelm

Advancements in high speed, light craft (HSLC) sea transportation require a main propulsion system that provides relatively high specific power with a minimum of weight/space. For commercial operations, the economics of the propulsion system are considered a key criterion in power plant selection. Marinizing a durable second generation industrial gas turbine, like the Solar Taurus® marine gas turbine, is ideally suited to satisfy the combination of the high vessel speed objective and the operating cost economic justification of commercial HSLC. Since the Taurus gas turbine has evolved from an earlier marine propulsion gas turbine and is in offshore platform service using materials and coatings resistant to marine environments, certification for marine prime propulsion concentrated primarily on operating inclination dynamic loading and the interfaces with the auxiliary support systems. With its high power to weight ratio, reliable performance, competitive first cost, and low operating costs, the Taurus marine industrial gas turbine can be further enhanced by recuperation and variable nozzle designs improving specific fuel consumption and part load efficiencies beyond other alternatives.


2008 ◽  
Vol 50 (3) ◽  
pp. 466-475 ◽  
Author(s):  
Alexander L. Bogorad ◽  
Justin J. Likar ◽  
Matthew P. Deeter ◽  
Kevin A. August ◽  
Graham P. Doorley ◽  
...  

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