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... 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 ...

... '''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 Atoll of the Marshall Islands. Though the vehicle lifted off with a ...

... the Sydney Australia based Tattersall's Club Magazine in October 1949. The 200' nuclear powered launch vehicle seems to predate other similar proposals for such a large rocket by Hermann Koelle at ... Willy Ley in his September 1949 book Conquest of the Moon . Image:1949-10-CRS-C-1.jpg border 200px Category:Launch Vehicle

... 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 ...

... . L. Taylor; C. M. Seaford '''JBIS Volume ''' - Contents of the Journal of the British Interplanetary Society for Volume 61 61 '''Page ''' - 128-138 '''Year''' - 2008 '''Keywords''' - Ares I Crew Launch Vehicle, aerodynamics, wind ... 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 ...

... Author - C.A. Carrouche '''Co-Author(s)''' - '''JBIS Volume ''' - Contents of the Journal of the British Interplanetary ... .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 ...

... 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 ... the launch vehicle and for launching. Image:EnergiaPolus.jpg Energia launch vehicle with the Polus spacecraft on the versatile stand-start complex being prepared for its first launch. Image:Energia1stlaunch.jpg The first launch of the Energia launch vehicle ...

Image:SVSLaunchStation.jpg 300px Saturn V Single Launch Space Station concept art (1967) (NASA) Category:Spacecraft

... statistics such as time in space, distance traveled, and mission objectives. Photographs and statistics for launch vehicles, orbiters, probes, and experimental equipment are featured in each equipment-specific reference. Covering such design ... 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 ...

... '''Page ''' - 32-38 '''Year''' - 2008 '''Keywords''' - Combustible launch vehicle, polyethylene tank '''JBIS Reference Code ''' - 2008.61.32 '''Number of Pages''' - 7 Abstract A single-stage launch vehicle equipped with a combustible tank shell of ... -thrust ratio are estimated under some assumptions concerning the obturator and compressor. Combustible launch vehicles are compared with conventional launch vehicles taking into consideration their payload mass ratios. Combustible launchers are preferable as small ...

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