Kármán line
The Kármán line is a conventional definition of the edge of space; it is widely but not universally accepted. The international record-keeping body FAI defines the Kármán line at an altitude of above mean sea level.
While named after Theodore von Kármán, who calculated a theoretical limit of altitude for aeroplane flight at above Earth, the later established Kármán line is more general and has no distinct physical significance, in that there is a rather gradual difference between the characteristics of the atmosphere at the line, and experts disagree on defining a distinct boundary where the atmosphere ends and space begins. It lies well above the altitude reachable by conventional airplanes or high-altitude balloons, and is approximately where satellites, even on very eccentric trajectories, will decay before completing a single orbit.
The Kármán line is mainly used for legal and regulatory purposes of differentiating between aircraft and spacecraft, which are then subject to different jurisdictions and legislations. While international law does not define the edge of space, or the limit of national airspace, most international organizations and regulatory agencies accept the FAI's Kármán line definition or something close to it. As defined by the FAI, the Kármán line was established in the 1960s. Various countries and entities define space's boundary differently for various purposes.
Definition
The FAI uses the term Kármán line to define the boundary between aeronautics and astronautics:Interpretations of the definition
The expressions "edge of space" or "near space" are often used to refer to a region below the boundary of Outer Space, which is often meant to include substantially lower regions as well. Thus, certain balloon or airplane flights might be described as "reaching the edge of space". In such statements, "reaching the edge of space" merely refers to going higher than average aeronautical vehicles commonly would.There is still no international legal definition of the demarcation between a country's air space and outer space. In 1963, Andrew G. Haley discussed the Kármán line in his book Space Law and Government. In a chapter on the limits of national sovereignty, he made a survey of major writers' opinions. He indicated the inherent imprecision of the Line:
In essence, the line represents a mean or "median" measurement. It is comparable to such measures used in the law as "mean sea level", "meander line", "tide line"; but it is more complex than these. In arriving at the von Kármán jurisdictional line, myriad factors must be considered – other than the factor of aerodynamic lift. These factors have been discussed in a very large body of literature and by a score or more of commentators. They include the physical constitution of the air; the biological and physiological viability; and still other factors which logically join to establish a point at which air no longer exists and at which airspace ends.
Kármán's comments
In the final chapter of his autobiography, Kármán addresses the issue of the edge of outer space:
Where space begins... can actually be determined by the speed of the space vehicle and its altitude above the Earth. Consider, for instance, the record flight of Captain Iven Carl Kincheloe Jr. in an X-2 rocket plane. Kincheloe flew 2000 miles per hour at 126,000 feet, or 24 miles up. At this altitude and speed, aerodynamic lift still carries 98 percent of the weight of the plane, and only two percent is carried by inertia, or Kepler force, as space scientists call it. But at 300,000 feet or 57 miles up, this relationship is reversed because there is no longer any air to contribute lift: only inertia prevails. This is certainly a physical boundary, where aerodynamics stops and astronautics begins, and so I thought why should it not also be a jurisdictional boundary? Andrew G. Haley has termed it the Kármán Jurisdictional Line. Below this line, space belongs to each country. Above this level there would be free space.
Technical considerations
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, 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, 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 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 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 current aircraft, namely the Bell X-2, and the maximum speed based on current 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 current 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
The U.S. Armed Forces definition of an astronaut is a person who has flown higher than above mean sea level, approximately the line between the mesosphere and the thermosphere. NASA formerly used the FAI's figure, though this was changed in 2005 to eliminate any inconsistency between military personnel and civilians flying in the same vehicle. Three veteran NASA X-15 pilots were retroactively awarded their astronaut wings, as they had flown between and during the 1960s, but at the time had not been recognized as astronauts. The latter altitude, achieved twice by Walker, exceeds the modern international definition of the boundary of space.The United States Federal Aviation Administration also recognizes this line as a space boundary:
Works by Jonathan McDowell and Thomas Gangale in 2018 advocate that the demarcation of space should be at, citing as evidence von Kármán's original notes and calculations, confirmation that orbiting objects can survive multiple perigees at altitudes around 80 to 90 km, plus functional, cultural, physical, technological, mathematical, and historical factors. More precisely, the paper summarizes:
These findings prompted the FAI to propose holding a joint conference with the International Astronautical Federation in 2019 to "fully explore" the issue.
Another definition proposed in international law discussions defines the lower boundary of space as the lowest perigee attainable by an orbiting space vehicle, but does not specify an altitude. This is the definition adopted by the U.S. military. Due to atmospheric drag, the lowest altitude at which an object in a circular orbit can complete at least one full revolution without propulsion is approximately. The U.S. government is resisting efforts to specify a precise regulatory boundary.