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... Korolev with R-7 on launch pad''' Image:R-7schematic.jpg R-7 rocket schematic Image:R-7facilities.jpg R-7 launch facilities Image:R-7preparation.jpg R-7 preparation Image:R-7lunar.jpg R-7 booster transportation of a four-stage launch vehicle R-7, plus rocket unit ... interplanetary station. Image:R-7lunarerector.jpg Four stage R-7 with lunar probe on erector Image:R-7pad.jpg R-7 on launch pad Image:R-7launch.jpg R-7 early launch Image:VostokR-7.jpg Vostok carrying R-7 launch vehicle Category:Launch Vehicle Category:Movie ...

... Author - L.D. Huebner et al '''Co-Author(s)''' - L. D. Huebner; R. M. Hall; D. A. Haynes; B. N. Pamadi; T. L. Taylor; C. M. Seaford '''JBIS ... Interplanetary Society for Volume 61 61 '''Page ''' - 128-138 '''Year''' - 2008 '''Keywords''' - Ares I Crew Launch Vehicle, aerodynamics, wind tunnel testing, computational fluid dynamics '''JBIS Reference Code ''' - 2008.61.128 '''Number of ... 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 ...

... 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 ...

... 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 ... RLV and proposes a payload of around 40 tonnes and a diameter of 7 meters. It explores three candidate systems Ariane 5 with enlarge payload fairing, an ...

... '''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 polyethylene ... -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 ...

... ''' - 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 ... 30 seconds the vehicle performed nominally. At T=+30 seconds, the main engine shut down. The vehicle landed 150 m downrange from the launch pad. Three days prior to the launch, a system test ...

... 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 ...

... 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 ...

... .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 ... it can easily be reconfigured into a reentry vehicle whilst in orbit. Having survived reentry but while still high in the atmosphere, the vehicle then divides into two separate components. Taking full ...

... , trajectory, launch vehicle, range maximization '''JBIS Reference Code ''' - 2008.61.395 '''Number of Pages''' - 6 Abstract This paper investigates a different way of finding the maximum range trajectory for a suborbital launch vehicle in ...

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