Works matching IS 00380946 AND DT 2014 AND VI 48 AND IP 7
Results: 22
On the reduction of dynamic loads during actuation of separation devices of advanced orbital astrophysical observatories.
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- Solar System Research, 2014, v. 48, n. 7, p. 475, doi. 10.1134/S0038094614070077
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Ultraviolet observatories of the future.
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- Solar System Research, 2014, v. 48, n. 7, p. 480, doi. 10.1134/S0038094614070181
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On the implementation of the program for exploration of Solar System small bodies.
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- Solar System Research, 2014, v. 48, n. 7, p. 485, doi. 10.1134/S0038094614070156
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Remote method of determining the coordinates of points on a planetary surface.
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- Solar System Research, 2014, v. 48, n. 7, p. 493, doi. 10.1134/S0038094614070028
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Final touchdown phases and a guidance and control methodology for a soft Moon landing.
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- Solar System Research, 2014, v. 48, n. 7, p. 497, doi. 10.1134/S0038094614070132
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Combined system for the compensation of the solar pressure-induced disturbing torque for geostationary satellites.
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- Solar System Research, 2014, v. 48, n. 7, p. 507, doi. 10.1134/S0038094614070193
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Joint computation of aerodynamic and radiation forces acting on spacecraft.
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- Solar System Research, 2014, v. 48, n. 7, p. 515, doi. 10.1134/S003809461407020X
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Ensuring dynamic stability of the orbital structure of the Arktika-M space system.
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- Solar System Research, 2014, v. 48, n. 7, p. 523, doi. 10.1134/S0038094614070168
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Near-Earth space as an object of global monitoring.
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- Solar System Research, 2014, v. 48, n. 7, p. 531, doi. 10.1134/S003809461407003X
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Using fracture mechanics principles for calculating the pressurized structure lifetime by example of the propellant tank for the fourth stage of launch vehicle VEGA.
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- Solar System Research, 2014, v. 48, n. 7, p. 536, doi. 10.1134/S0038094614070053
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Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project.
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- Solar System Research, 2014, v. 48, n. 7, p. 541, doi. 10.1134/S0038094614070089
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A sensor for the spatial registration and measurement of particles parameters in near and deep space-Experimental investigation of SiO-aerogel characteristics.
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- Solar System Research, 2014, v. 48, n. 7, p. 549, doi. 10.1134/S0038094614070090
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Quality analysis of image geolocation for a space synthetic aperture radar.
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- Solar System Research, 2014, v. 48, n. 7, p. 555, doi. 10.1134/S0038094614070235
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Baroresistor effect and semiconductor thin-film baroresistors based on samarium sulfide for spacecraft applications.
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- Solar System Research, 2014, v. 48, n. 7, p. 561, doi. 10.1134/S0038094614070107
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A method for a short-term forecast of the absorbed dose accumulation dynamics on the international space station based on radiation monitoring system data.
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- Solar System Research, 2014, v. 48, n. 7, p. 568, doi. 10.1134/S0038094614070144
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A navigation method for an automated interplanetary probe on a quasi-satellite orbit in a three-body problem based on optical measurements.
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- Solar System Research, 2014, v. 48, n. 7, p. 574, doi. 10.1134/S0038094614070065
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A strategy for developing a launch vehicle system for orbit insertion: Methodological aspects.
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- Solar System Research, 2014, v. 48, n. 7, p. 582, doi. 10.1134/S0038094614070119
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Problem '13' for geostationary spacecraft.
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- Solar System Research, 2014, v. 48, n. 7, p. 588, doi. 10.1134/S003809461407017X
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Rings of debris in near-Earth space.
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- Solar System Research, 2014, v. 48, n. 7, p. 593, doi. 10.1134/S0038094614070041
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Perturbing effect of solar radiation on the Spektr-RG spacecraft in operational orbit.
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- Solar System Research, 2014, v. 48, n. 7, p. 601, doi. 10.1134/S0038094614070211
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Optimization of the transfer trajectory of a low-thrust spacecraft for research of Jupiter using an Earth gravity-assist maneuver.
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- Solar System Research, 2014, v. 48, n. 7, p. 606, doi. 10.1134/S0038094614070120
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Science issues of the 'Spektr-UF' project.
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- Solar System Research, 2014, v. 48, n. 7, p. 467, doi. 10.1134/S0038094614070223
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