 space launch is the earliest part of a flight that reaches space. space launch involves liftoff, when a rocket or other space launch vehicle leaves the ground, floating ship or midair aircraft at the start of a flight. liftoff is of two main types: rocket launch (the current conventional method), and non-rocket spacelaunch (where other forms of propulsion are employed, including airbreathing jet engines or other kinds). ==issues with reaching space== ===definition of space=== space has no physical edge to it as the atmospheric pressure gradually reduces with altitude; instead, the edge of space is defined by convention, often the kÃ¡rmÃ¡n line of 100&nbsp;km. other definitions have been created as well, in the us for example space has been defined as 50 miles. ===energy=== therefore, by definition for spaceflight to occur, sufficient altitude is necessary. this implies a minimum specific gravitational potential energy needs to be overcome: for the kÃ¡rmÃ¡n line this is approximately 10 mj/kg. w=mgh, m=1&nbsp;kg, g=9.82&nbsp;m/s2, h=106m. w=1*9.82*106â107j/kg=10mj/kg in practice, a higher energy than this is needed to be expended due to losses such as airdrag, propulsive efficiency, cycle efficiency of engines that are employed and gravity drag. what we have in the past fifty years usually meant, though, by spaceflight has included remaining in space for a period of time, rather than going up and immediately falling back to earth. this entails orbit, which is, at altitudes prevalently entered by such means, not a matter of altitude, but rather of velocity, which is not to say that we need not discuss air friction and relevant altitudes in relation to that and orbit. at much, much, higher altitudes than many orbital ones maintained by satellites, altitude begins to become a larger and larger factor and speed a lesser one. at lower altitudes, due to the high speed required to remain in orbit, air friction is a very important consideration affecting satellites, much more than in the popular image of space. at even lower altitudes, balloons, with no forward velocity, can serve many of the roles satellites play. ===g-forces=== many cargoes, particularly humans have a limiting g-force that they can survive. for humans this is about 3-6 g. some launchers such as gun launchers would give accelerations in the hundred or thousands of g and thus are completely unsuitable. ===reliability=== launchers vary with respect to their reliability for achieving the mission. ===safety=== safety is the probability of causing injury or loss of life. unreliable launchers are not necessarily unsafe, whereas reliable launchers are usually, but not invariably safe. apart from catastrophic failure of the launch vehicle itself other safety hazards include depressurisation, and the [[van allen radiati
Spaceflight_concepts