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Displaying 1—10 of 1000 matches for query "The_Feng_Bao-1_Launch_Vehicle_Programme" retrieved in 0.026 sec with these stats:

  • "the" found 506431 times in 20587 documents
  • "feng" found 16 times in 8 documents
  • "bao" found 5 times in 3 documents
  • "1" found 54409 times in 16881 documents
  • "launch" found 30905 times in 9663 documents
  • "vehicl" found 10011 times in 4664 documents
  • "programm" found 500 times in 230 documents



... '''Keywords''' - Feng Bao -1, Ji Shu Shiyan Weixing , Shi Jian '''JBIS Reference Code ''' - 2002.55.226 '''Number of Pages''' - 10 Abstract This paper provides a review of the little-described Feng Bao-1 launch vehicle and the satellite launches which took place during 1973-1981. Details are given of the launch vehicle's development and flight history, as well as numerical data for the launch vehicle itself. The satellites which were launched by the vehicle ...
... Abstract A companion paper has reviewed the various series of satellites launched using the small Cosmos-2/2M vehicle during 1961- 1977 1 . The present paper presents a review of the orbital data for these satellite groups ... click http://www.jbis.org.uk/paper.php?p=1999.52.127 here ''' ---- Journal of the British Interplanetary Society JBIS is © 1934-2013 http://www.bis-space.com British Interplanetary Society ...
... of the British Interplanetary Society for Volume 60 60 '''Page ''' - 289-293 '''Year''' - 2007 '''Keywords''' - Falcon 1, launch vehicle, low cost launch '''JBIS Reference Code ''' - 2007.60.289 '''Number of Pages''' - 5 Abstract Falcon 1 was launched on March 25, 2006 from Omelek, a small island which is part of the Kwajalein ...
... Mission Directorate (ESMD), the Ares Projects Office at the NASA Marshall Space Flight Center was assigned project management responsibilities for the design and development of the first vehicle in the architecture, the Ares I Crew Launch Vehicle (CLV), which will be used to launch astronauts to low earth orbit and rendezvous with either the International Space Station or the ...
... of the Energia-M launch vehicle is accomplished on the transport-erecting assembly of the Energia launch vehicle. Image:Energiatransporter.jpg Transportation of the Energia launch vehicle Image:EnergiaPolustransporte.jpg Transportation of the Energia launch vehicle with the Polus spacecraft on the external suspension to the versatile stand-start complex. Image:EnergiaMonpad.jpg The Energia-M launch vehicle ...
... at the mechanism that gets it all started describes 259 types of launch vehicles developed by China, the European Space Agency , Japan, Russia, and the United States. A total of 259 types of launch vehicles have been launched into space by the United States (165), Russia ...
... ''' - 2003 '''Keywords''' - Launch systems, heavy lift launcher, reusable launch vehicle '''JBIS Reference Code ''' - 2003.56.369 '''Number of Pages''' - 9 Abstract A Reusable Launch Vehicle (RLV) should be sized to minimise the specific launch costs and this probably means a payload around 10 tonnes and the 4.5 m diameter envelope, both similar to the Space Shuttle ...
... field in the gasification chamber, estimating gasification rate of polyethylene, launch vehicle shortening rate and area of gasification. Experimental determination of the gasification rate is described. The gasification chamber specific mass as well as the propulsion plant weight-to-thrust ratio are estimated under some assumptions concerning the obturator and compressor. Combustible launch vehicles are compared with conventional launch vehicles taking into ...
Image:SSTO MSFC-1961.jpg 300px Single Stage to Orbit launch vehicle concept (1961) MSFC Category:Launch Vehicle
... of the Journal of the British Interplanetary Society for Volume 52 52 '''Page ''' - 169-174 '''Year''' - 1999 '''Keywords''' - '''JBIS Reference Code ''' - 1999.52.169 '''Number of Pages''' - 6 Abstract A recoverable Orbital Launch Vehicle is proposed configured along the lines of a commercially successful, expendable launch vehicle. The reuseable lower stage is comprised of a single, Space Shuttle Solid Rocket Booster. The upper stage is propelled ...

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