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Displaying 1—10 of 1000 matches for query "Archibald_Montgomery_Low" retrieved in 0.002 sec with these stats:

  • "archibald" found 22 times in 16 documents
  • "montgomeri" found 45 times in 40 documents
  • "low" found 4946 times in 3607 documents



... Infobox bodystyle = float:right; valign:top; title = G. David Low titlestyle = image = Image:Astronaut_low.jpg 200px imagestyle = caption = G. David Low captionstyle = headerstyle = background: ccf; labelstyle = background: ddf; datastyle = text-align:right; header1 = label1 = data1 = header2 = label2 = Birth Name data2 = G. David Low header3 = label3 = Birth Date data3 = Feb 19 1956 header4 = label4 = Birth Place data4 = label5 = Date ...
... British Interplanetary Society for Volume 59 59 '''Page ''' - 158-166 '''Year''' - 2006 '''Keywords''' - Small Satellite, Low-Cost, Radar, SAR, DMC '''JBIS Reference Code ''' - 2006.59.158 '''Number of Pages''' - 9 Abstract ... the Disaster Monitoring Constellation (DMC). During this period we have demonstrated the utility of a low-cost satellite system that uses optical sensors and is capable of providing daily imaging globally ...
... been conventional missions where the solar sail is utilised primarily as a means of efficient, low thrust propulsion for orbit transfer. For this reason solar sailing has historically been neglected in ... at lower cost than with electric or chemical propulsion. In this paper some of these low cost, high energy missions will be reviewed. In particular, new families of non-Keplerian orbits ...
... British Interplanetary Society for Volume 61 61 '''Page ''' - 139-145 '''Year''' - 2008 '''Keywords''' - Trajectory optimization, low-thrust, optimal control, non-linear programming, guidance '''JBIS Reference Code ''' - 2008.61.139 '''Number of ... the minimum-time transfer between two orbits, including the phasing with a desired spacecraft. Very-low thrust means several hundred revolutions to perform the large change in orbital elements. The optimal ...
... Volume 62 62 '''Page ''' - 15-31 '''Year''' - 2009 '''Keywords''' - Finite elements in time, trajectory optimisation, low-thrust multigravity assist trajectories, direct transcription methods, global optimisation methods '''JBIS Reference Code ''' - 2009.62 ... on Finite Elements in Time was used for the design and optimisation of the entire low-thrust gravity assist transfer from the Earth to Europa. Prior to that, a global search ...
... are briefly described. High resolution IDES model simulations of the historical debris environment evolution in Low Earth Orbit (LEO) are then presented for centimetre and decimetre object size thresholds. The simulated ...
... the expected imagery received. The aim of the design process was to produce a practical, low-cost, small satellite mission with mainly commercial off-the-shelf components and a rapid development ...
... uncomfortable to use. Recent studies suggest that exposing the body to short periods (
REDIRECT G. David Low Category:Astronaut-Cosmonaut
REDIRECT G. David Low

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