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18篇 您的检索式:作者名="Vulpetti"
    题名 作者 年代 出处 被引量
13D high-speed escape heliocentric trajectories by all-metallic-sail low-mass sailcraft显示文摘Vulpetti G 0,,1:1
2Structural characterization of the GSK-3β active site using se- lective and non-selective ATP-mimetic inhibitors显示文摘BERTRAND J A THIEFFINE S VULPETTI A 2003J Mol Biol2003,333,:1
33D high-speed escape he-liocentric trajectories by all-metallic-sail low-mass sailcraft显示文摘Vulpetti G 0,,1:1
4Sequence and structural analysis of kinase ATP pocket residues 显示文摘Vulpetti A Bosotti R 2004I1 Farmaco2004,59,:1
5Sequence and structural analysis of kinase ATP pocket residues显示文摘Vulpetti A Bosotti R 0,,10:1
6Structural characterization of the GSK-3beta active site using selective and non-selective ATP-mimetic inhibitors显示文摘Bertrand J A Thieffine S Vulpetti A 2003J Mol Biol2003,333,:1
7Sequence and structural analysis of kinase ATP pocket residues显示文摘Anna Vulpetti Roberta Bosotti 2004Il Farmaco2004,,10:1
8Sailcraft at high speed by orbital angular momentum reversal 显示文摘Vulpetti G 1997Acta Astronautica1997,40,10:1
93D high speed escape heliocentric trajectories by all metallic-sail low-mass saileraft 显示文摘Vulpetti G 1996Acta Astronautica1996,39,:1
10Sailcraft at high speed by orbital angular momentum reversal 显示文摘Vulpetti G 1997Acta Astronautica1997,40,10:1
11Predicting polypharmacology by binding site similarity: from kinases to the protein universe 显示文摘Milletti F Vulpetti A 2010J Chem InfModel2010,50,8:1
12The Aurora Project : Removal of Plastic Substrate to Obtain an All-Metal Solar Sail 显示文摘Scaglione Vulpetti 1999Acta Astronautica1999,44,24:1
13显示文摘BERSTRAND J A THIEFFINE S VULPETTI A 2003J Mol Biol2003,333,:1
143D high-speed escape heliocentric trajectories by all-metallic-sail low mass sailcraft 显示文摘Vulpetti G 1996Acta Astronautica1996,39,14:1
15The Aurora Project:Removal of Plastic Substrate to Obtain an All-Metal So-lar Sail显示文摘S. Scaglione G. Vulpetti 0,,2:1
16Solar sail H-reversal trajectory:A review of its advances and applications显示文摘The set of the orbital angular-momentum reversal,or H-reversal,sailcraft trajectory was born as a type of unconventional precursor interstellar mission trajectory by using highperformance solar sails.Starting from an outline of the H-reversal sail trajectory,this paper mainly focuses on the 2D reversal-mode solution to the general solar-photon sail motion equations.The feasible region for H-reversal trajectories in fixed sail attitude angles is illustrated.Some interesting applications of the H-reversal trajectory are presented in detail to show its advantages.As a special case,a precursor interstellar probe can be delivered with a constant sail orientation in the H-reversal trajectory to be compared with the direct-motion sail flyby of the Sun.Of importance are the heliocentric periodic orbits in double H-reversal modes,obtained via both fixed and time-varying sail attitude angles.Two more applications involving H-reversal trajectories are discussed in terms of asteroid deflection and transfer trajectory to rectilinear orbits.Finally,some items of the mathematics behind the 3D motion-reversal trajectories are summarized.Xiangyuan Zeng Giovanni Vulpetti Christian Circi 2019Astrodynamics2019,3,1:0
17Message from the Guest Editors of the Special Issue on Solar-Photon Space Sailing显示文摘Since the 1960s,an increasing interest in space propulsion methods(a)not-high-limited in energy(e.g.,electric rocket propulsion)and(b)involving no propellant(space sailing),has been advancing from theoretical,numericalsimulation,and technological viewpoints.In particular,among the propulsion concepts of type(b),solar-photon sailing(SPS)has received greater and greater attention.Giovanni Vulpetti Christian Circi Xiangyuan Zeng 2019Astrodynamics2019,3,3:0
18Message from the Guest Editors of the Special Issue on Astrodynamics and Engineering Aspects of Hayabusa2-Sample Return Mission to the Asteroid Ryugu显示文摘Dear authors and readers,Since the beginning of the space age,the return of samples from the other celestial bodies has been deemed one of the ultimate forms of unmanned robotic missions.Realizing a sample return mission requires profound knowledge of many wide and different areas of engineering and science.In a special way,astrodynamics plays a crucial role throughout the mission,ranging from accurate guidance and navigation to distant bodies,to precise modeling of dynamical environment of target bodies,precision landing to an aimed point,various surface and proximity activities around the bodies,and orbit design for the round-trip journey.Yuichi Tsuda Xiangyuan Zeng Christian Circi Giovanni Vulpetti 2020Astrodynamics2020,4,2:0
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