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22 search results for "performance"
21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft
Aerothermal performance and structural integrity of a René-41 thermal protection system at Mach 6.6 / W.
1.1.2016 Solid Rocket Motors Developed by DO-5
The basic technical problems are considered, solution of which allowed building the main motors and dispensing motors with high performance level and highly-effective rocket [...]
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9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands
It was concluded that experiments on error measurements can be replaced with calculations for those parameters which have sufficient initial data on metrological performance [...]
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6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points
The obtained test data is analyzed, and conclusions are drawn on the effect of different factors on joint performance including force action on ILV in disconnection.
8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation
2019, (1); 54-63 DOI: https://doi.org/10.33136/stma2019.01.054 Language: Russian Annotation: This paper describes the effective approach for the technology of the rocket airframe [...]
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7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants
The important steps were the development of methodology for pressurization system parameters calculation, which enabled achievement of the substantial improvements of their [...]
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5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime
In different countries they have their own characteristics, depending on the type and performance of the launch vehicles, infrastructure features (geography of the site, [...]
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2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg
Angular motion with nominal and perturbed performances of the aircraft and flight conditions has been consistently considered.
21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position
It results in the decrease of the required pressurization gas volume, which boosts reduction of the performance of the launch vehicle as a whole.
19.1.2019 Peculiarities of Radio Transparent Fairings Development
Basic principles of radiotransparent radomes development and aspects of ceramic shells coupling with structural rings are considered, as well as the results of strength analyses and [...]
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