No atmosphere abruptly ends, instead becoming progressively less dense with altitude. Depending on how the various layers that make up the space around the
Earth are defined (and depending on whether these layers are considered part of the actual atmosphere), the definition of the edge of space could vary considerably: If one were to consider the
thermosphere and
exosphere part of the atmosphere and not of space, one might have to extend the boundary of space to at least above sea level. The Kármán line thus is a largely arbitrary definition based on some technical considerations. An aircraft can stay aloft only by constantly traveling forward relative to the air (rather than the ground), so that the wings can generate aerodynamic lift. The thinner the air, the faster the plane must go to generate enough lift to stay up. At very high speeds, centrifugal force (Kepler force) contributes to maintaining altitude. This is the virtual force that keeps satellites in circular orbit without any aerodynamic lift. As altitude increases and air density decreases, the speed to generate enough aerodynamic lift to support the aircraft weight increases until the speed becomes so high that the centrifugal force contribution becomes significant. At a high enough altitude, the centrifugal force will dominate over the lift force and the aircraft would become effectively an orbiting spacecraft instead of an aircraft supported by aerodynamic lift. In 1956, von Kármán presented a paper in which he discussed aerothermal limits to flight. The faster aircraft fly, the more heat they would generate due to
aerodynamic heating from friction with the atmosphere and
adiabatic processes. Based on the then-current
state of the art, he calculated the speeds and altitudes at which continuous flight was possible—fast enough that enough lift would be generated and slow enough that the vehicle would not overheat. The chart included an inflection point at around , above which the minimum speed would place the vehicle into
orbit. The term "Kármán line" was invented by
Andrew G. Haley in a 1959 paper, based on the chart in von Kármán's 1956 paper, but Haley acknowledged that the limit was theoretical and would change as technology improved, as the minimum speed in von Kármán's calculations was based on the speed-to-weight ratio of existing aircraft, namely the
Bell X-2, and the maximum speed based on cooling technologies and heat-resistant materials. Haley also cited other technical considerations for that altitude, as it was approximately the altitude limit for an
airbreathing jet engine based on existing technology. In the same 1959 paper, Haley also referred to as the "von Kármán Line", which was the lowest altitude at which
free-radical atomic oxygen occurred. == Alternatives to the FAI definition ==