Here's Some Definitions I found:
Outer Space
'''Outer space''' (also called just ''space''), as a name for a region, refers to the relatively empty parts of the
Universe, outside the
celestial body's atmosphere atmospheres of celestial bodies. The term ''outer space'' is used to distinguish it from
airspace and terrestrial locations. As
Earth's atmosphere has no abrupt cut-off, but rather thins gradually with increasing altitude, there is no definite boundary between the atmosphere and space. The altitude of 100 kilometers or 62 miles established by the
Federation Aeronautique Internationale is the most widely used definition as the boundary between atmosphere and space. In the United States, persons who travel above an altitude of 50 miles (80 kilometers) are designated as
Astronaut astronauts. 400,000 feet (75 miles or 120 kilometers) marks the boundary where atmospheric effects become noticeable during
re-entry. (See also
Karman line.)
Milestones on the way to space
*4.6 km (15,000 ft) -
FAA requires supplemental oxygen for aircraft pilots and passengers *5.3 km (17,400 ft) - Half of the earth's atmosphere is below this altitude *16 km (52,500 ft) - Pressurized cabin or pressure suit required *18 km (59,000 ft) - Upper limit of the
Troposphere *20 km (65,600 ft) - Water at room temperature boils without a pressurized container (the popular notion that bodily fluids would start to boil at this point is false because the confines of the body generate enough pressure to prevent actual boiling) *24 km (78,700 ft) - Regular aircraft pressurization systems no longer function *32 km (105,000 ft) -
Turbojets no longer function *45 km (148,000 ft) -
Ramjets no longer function *50 km (164,000 ft) -
Stratosphere ends *80 km (262,000 ft) -
Mesosphere ends *100 km (328,000 ft)-
airfoil Aerodynamic surfaces no longer function Reentry from orbit begins at 122 km (400,000 ft).
Space does not equal orbit
A common misunderstanding about the boundary to space is that
orbit occurs by reaching this altitude. Orbit, however, requires
orbital speed and can theoretically occur at any altitude. Atmospheric drag precludes an orbit that is too low. Minimal altitudes for a stable orbit begin at around 350 km (220 miles) above mean sea level, so to actually perform an
orbital spaceflight, a spacecraft would need to go higher and (more importantly) faster than what would be required for a
sub-orbital spaceflight. Reaching orbit requires tremendous speed. A craft has not reached orbit until it is circling Earth so quickly that the upward
centrifugal force centrifugal "force" cancels the downward
gravity gravitational force on the craft. Having climbed up out of the atmosphere, a craft entering orbit must then turn sideways and continue firing its rockets to reach the necessary speed; for
low Earth orbit, the speed is about 7.9 km/s (18,000 mph). Thus, achieving the necessary altitude is only the first step in reaching orbit. The energy required to reach velocity for low earth orbit (32 MJ/kg) is about twenty times the energy to reach the corresponding altitude (10 kJ/km/kg).
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Outer space (also called just
space) as a name for a region, refers to the relatively empty parts of the
Universe, outside the
atmospheres of celestial bodies. The term
outer space is used to distinguish it from
airspace and terrestrial locations. Although outer space is certainly
spacious, it is now known to be far from empty, and filled with a tenuous
plasma.
As
Earth's atmosphere has no abrupt cut-off, but rather thins gradually with increasing altitude, there is no definite boundary between the atmosphere and space. The altitude of 100 kilometers or 62 miles established by the
Federation Aeronautique Internationale is the most widely used definition as the boundary between atmosphere and space. In the United States, persons who travel above an altitude of 50 miles (80 kilometers) are designated as
astronauts. 400,000 feet (75 miles or 120 kilometers) marks the boundary where atmospheric effects become noticeable during
re-entry.
Milestones on the way to space
- 4.6 km (15,000 ft) - FAA requires supplemental oxygen for aircraft pilots and passengers
- 5.3 km (17,400 ft) - Half of the earth's atmosphere is below this altitude
- 16 km (52,500 ft) - Pressurized cabin or pressure suit required
- 18 km (59,000 ft) - Upper limit of the Troposphere
- 20 km (65,600 ft) - Water at room temperature boils without a pressurized container (the popular notion that bodily fluids would start to boil at this point is false because the confines of the body generate enough pressure to prevent actual boiling)
- 24 km (78,700 ft) - Regular aircraft pressurization systems no longer function
- 32 km (105,000 ft) - Turbojets no longer function
- 45 km (148,000 ft) - Ramjets no longer function
- 50 km (164,000 ft) - Stratosphere ends
- 80 km (262,000 ft) - Mesosphere ends
- 100 km (328,000 ft)- Aerodynamic surfaces no longer function
Reentry from orbit begins at 122 km (400,000 ft).
A common misunderstanding about the boundary to space is that
orbit occurs by reaching this altitude. Orbit, however, requires
orbital speed and can theoretically occur at any altitude. Atmospheric drag precludes an orbit that is too low.
Minimal altitudes for a stable orbit around the Earth begin at around 350 km (220 miles) above mean sea level, so to actually perform an
orbital spaceflight, a spacecraft would need to go higher and (more importantly) faster than what would be required for a
sub-orbital spaceflight.
Reaching orbit requires tremendous speed. A craft has not reached orbit until it is circling Earth so quickly that the upward
centrifugal "force" cancels the downward
gravitational force on the craft. Having climbed up out of the atmosphere, a craft entering orbit must then turn sideways and continue firing its rockets to reach the necessary speed; for
low Earth orbit, the speed is about 7.9 km/s (18,000 mph). Thus, achieving the necessary altitude is only the first step in reaching orbit.
The energy required to reach velocity for low earth orbit (32 MJ/kg) is about twenty times the energy to reach the corresponding altitude (10 kJ/km/kg).