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... -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 ...

... '''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 ... the overall acquisition cost. Using a Heavy Lift Vehicle (HLV) with high specific launch costs but able to launch the system in one piece would lead to lower overall acquisition costs. The ...

... propulsion. Solid propellants do not require as much fuel- chamber strengthening to withstand a hypervelocity launch as do liquid propellants, but traditional solid fuels have lower exhaust velocities than liquid hydrogen ... . The shock-stability of frozen hydrogen/frozen oxygen propellant has been experimentally demonstrated. A hypervelocity launch system using frozen hydrogen/frozen oxygen propellant would be a revolutionary new development in spaceflight ...

... 60 60 '''Page ''' - 249-256 '''Year''' - 2007 '''Keywords''' - Small satellites, French satellites history, launch systems, piggy-back launch '''JBIS Reference Code ''' - 2007.60.249 '''Number of Pages''' - 8 Abstract After an historical ... the lessons learned from this extensive range of launch experiences, which include piggy-back configurations on Ariane 4 and 5, Russian launches and US launches. Our launcher choices for coming missions will then ...

... 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 ... main engine shut down. The vehicle landed 150 m downrange from the launch pad. Three days prior to the launch, a system test was conducted which included a static firing of the ...

... the British Interplanetary Society for Volume 60 60 '''Page ''' - 54-62 '''Year''' - 2007 '''Keywords''' - Electromagnetic, launch, space '''JBIS Reference Code ''' - 2007.60.54 '''Number of Pages''' - 9 Abstract Many advances in ... US, European, Russian, and Chinese researchers. An intermediate step proposed in France could be to launch payloads to sounding rocket altitudes for ionospheric research. '''To BUY this paper click http://www ...

... of polyethylene, calculating quasisteady temperature 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 ... -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 ...

We launch from Florida. Other nations have different launch sites. The Mojave Desert is a good bet for launch systems initially carried aloft by an aircraft, then launched. Anything that launches vertically will be from ... big difference between launching to orbit and just launching to touch the edge of space and tumble back down. Due to launch frequency to go to the space hotels, the launch areas will have ...

... , the aforementioned agency holding all of the criteria for that meaning. Back in 2013, Azercosmos launched its first ever satelliteAzerspace-1 telecommunication satellite with two communication payloads: Ku-Band and C ... based Orbital Service Corporation manufactured the first satellite of the Azerbaijan Republic. Azerspace-1 was launched by Ariane-5ECA of Arianespace which belongs to the French Space Agency,The objective lies ...

... for Volume 58 58 '''Page ''' - 302-309 '''Year''' - 2005 '''Keywords''' - Manned Mars missions, medium-lift launch systems '''JBIS Reference Code ''' - 2005.58.302 '''Number of Pages''' - 8 Abstract A method of accomplishing manned expeditions to Mars with existing medium-lift launch systems is discussed. In this architecture, 20-tonne propulsion stages are placed individually in low ...

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