Search wiki using Sphinx

Jump to: navigation, search

... of the British Interplanetary Society for Volume 62 62 '''Page ''' - 162-174 '''Year''' - 2009 '''Keywords''' - Titan, mission design, aerocapture, balloon '''JBIS Reference Code ''' - 2009.62.162 '''Number of Pages''' - 13 Abstract ... of vehicle types including orbiters, landers, boats, airplanes, balloons and penetrators. Particularly recurrent themes in Titan exploration are the use of multiple platforms to address a wide range of scientific goals ...

... British Interplanetary Society for Volume 61 61 '''Page ''' - 118-124 '''Year''' - 2008 '''Keywords''' - Titan UAV, Titan surface exploration, Titan aeronautics '''JBIS Reference Code ''' - 2008.61.118 '''Number of Pages''' - 7 Abstract A concept ... imagery, boundary-layer meteorological profiles and other data. The cold, thick atmosphere on low-gravity Titan makes a fixed- or moving-wing vehicle easy to fly, but requires substantial energy to ...

... British Interplanetary Society for Volume 61 61 '''Page ''' - 295-299 '''Year''' - 2008 '''Keywords''' - Cassini mission, Titan, Titan Radar Mapper '''JBIS Reference Code ''' - 2008.61.295 '''Number of Pages''' - 5 Abstract Several flybys of Titan have been successfully performed by the Cassini spacecraft. Among its instruments is a radar mapper ...

... 63 63 '''Page ''' - 9-14 '''Year''' - 2010 '''Keywords''' - Radioisotope power, Stirling Generator, Convective Heat transfer, Titan '''JBIS Reference Code ''' - 2010.63.9 '''Number of Pages''' - 6 Abstract Like other energy conversion ... Radioisotope Generator (ASRG) in the dense, cold atmosphere of Titan. We find the power output of an ideal RPS in the Titan environment could be considerably superior to that in space vacuum ...

... Code ''' - 2000.53.218 '''Number of Pages''' - 17 Abstract The likely scientific questions posed by Titan after the upcoming Cassini mission, and the engineering issues associated with the platforms required for ... structural challenges. Airships and helicopters appear to be quite feasible, given several advantageous aspects of Titan's environment, and would satisfy the broadest range of scientific objectives. '''To BUY this paper ...

... of the British Interplanetary Society for Volume 61 61 '''Page ''' - 2-13 '''Year''' - 2008 '''Keywords''' - Titan, balloon, radioisotope power '''JBIS Reference Code ''' - 2008.61.2 '''Number of Pages''' - 12 Abstract Concepts for lighter-than-air exploration of Titan are reviewed. Logical vehicle designs with existing power sources (primary batteries, or 100 We-class ...

... .gsfc.nasa.gov/nmc/datasetSearch.do?spacecraft=LAGEOS%20II Here Carrier_Rocket = Space Shuttle LAGEOS II (LAser GEOdetic Satellite) was a very dense (high mass-to-area ratio) laser retroreflector satellite ... with appropriate laser-tracking systems (about 16 mobile and 10 fixed laser-ranging facilities), LAGEOS II permitted extreme precision ranging measurements for both geometric mode (multilateration) and orbital dynamic mode determinations ...

... = 1996-065B Webpage = Semimajor_Axis = Eccentricity = Inclination = Orbital_Period = Apoapsis = Periapsis = Orbits = Alternate Names = ORFEUS II, STS 80/ ORFEUS, 24661 Experiments = Nominal Power = Additional Information = http://nssdc.gsfc.nasa.gov/nmc ... . The Interstellar Medium Absorption Profile Spectrograph (IMAPS) was operated independently from ORFEUS. The ORFEUS-SPAS II mission was flown in November-December 1996. The mission acquired spectra of numerous celestial objects ...

... : ddf; datastyle = text-align:right; header1 = label1 = data1 = header2 = label2 = Birth Name data2 = Bruce McCandless II header3 = label3 = Birth Date data3 = Jun 8 1937 header4 = label4 = Birth Place data4 = label5 = Date ... -102) from December 1960 to February 1964, flying the Skyray and the F-4B Phantom II, and he saw duty aboard the USS FORRESTAL (CVA-59) and the USS ENTERPRISE (CVA ...

Media:GT03_PAO.PDF Flight transcript Gemini Titan 3 March 23 1965 Category:Publications

Powered by Sphinx