About the upper atmosphere , the way in and out and the differences in temperature that are found to be symmetrical, in that they indicate some
larger similarity with patterns and their indications of the light change previous to the earth's blue color as seen from positions beyond earth in relation to faster than light speed interactions. Also some facts of "Kennedy's dream" and the project of "super massive" concepts of space ships, whatever that means, when you use the, "senator moon beam approach" some scifi science may actually be real concepts thought about by other thinkers such as Kennedy, "the first of the popular scifi scientists together with Arthur C. Clarke who invented the "satellite" and it was this that Kennedy was using when he made his speech about going to the moon. Arthur C. Clarke was writing about concepts of the space age long ago, he invented most of the things in use today and his most famous invention is the satellite. Imagine that, some 60 years ago. I actually owned this book as a kid together with ,"the high fronteir " by Gerard O'neil who predicts the scifi science of living in sustainable space stations the size of small countries. So these are probably the best scifi scientists that ever lived. |
image credit:
goodreads.com |
image credit;thermosphere
assignement point
When you're so high up in the earth's atmosphere, you are in fact in the coldest place related to earth. So you would quickly freeze and become hard.
The facts of earth's ground level ,lowest temperature is about -60 C.
It is where the inuit eskimoes live at the coldest part of the year.
So it is because of this cold region above earth as the the thermosphere , that "spaceships doing re entry into earth's atmosphere, start to displace through it and the friction created as motion against the cold particles= the heating of the "lower temperature state of water as H2O ( fluid) change to gaseous.
The basics of this region, defines oxygen in motion at such a low velocity that the similarity to the coldness of space, will displace light at it's basic velocity as the speed of light.
When the speed of light is reduced by "alternating cold" in space as the upper atmosphere of earth, the light will decelerate to the velocity that may be computed as
Here is the temperature of space:
As you probably know, space is already very, very cold — roughly 2.7 Kelvin (-270.45 Celsius, -454.81 Fahrenheit). This is mostly due to a lack of atmosphere and the vacuum-like nature of space — with very few molecules to energetically bounce around, there can be no heat
c (velocity) of light in the -270.45 C
and the "new" velocity of light in the -90 C
as:
1/-90 x -270=3
or as:
1/ -270 x -90
=0,3333 of the speed of light.
The speed of light =
299 792 458 m / s
So then, 0,333 % must be equal to
299 792 460 , 99779246 km / sec
This defines the motion of light along the upper atmosphere as the change of the temperature by an amount equal to
-270.45--90
=180
as the basics of the change of the angle of the earth's atmosphere as the 180 degree constant.
So along this curvature, the light may displace into the shadow side of the earth and continue to
360 degrees.
So then the difference in temperature as the 2x 180 =360 degrees ,the multiple as shared becomes
= 90 degrees as the right angle of the shift of the day time atmosphere to the night time atmosphere.
So then the change in temperature must be related to earth's surface as the "mean temperature " = zero degrees C.
Meaning that the change in temperature may also faze to the -90 by the 180 as the change in light as related to
the x2 multiple of the speed of light in this faze change of 180 degrees as,
299 792 460 .9977 x2=599 584 741.994.
Meaning beyond the speed of light as the blue shift in this layer of the 180 degrees to the reduction into 90
degrees as the measure need for any x and y measure to have the prerequisites to make any equation with
light to be computable as physics.
here are some really suprising values of the speed of light as related to the temperature of the earth's atmospherical layers that generate
faster than light velocities.
The strange facts are that the temp change= 90 to 180 to 270 to 360.
So to does there need be some way that the temperature interacts on the basics of reentry into earth's atmosphere by being as such
90 x1c , 180 x 2c, 270 xc3 and c delta as 360
assignement point
When you're so high up in the earth's atmosphere, you are in fact in the coldest place related to earth. So you would quickly freeze and become hard.
The facts of earth's ground level ,lowest temperature is about -60 C.
It is where the inuit eskimoes live at the coldest part of the year.
So it is because of this cold region above earth as the the thermosphere , that "spaceships doing re entry into earth's atmosphere, start to displace through it and the friction created as motion against the cold particles= the heating of the "lower temperature state of water as H2O ( fluid) change to gaseous.
The basics of this region, defines oxygen in motion at such a low velocity that the similarity to the coldness of space, will displace light at it's basic velocity as the speed of light.
When the speed of light is reduced by "alternating cold" in space as the upper atmosphere of earth, the light will decelerate to the velocity that may be computed as
Here is the temperature of space:
As you probably know, space is already very, very cold — roughly 2.7 Kelvin (-270.45 Celsius, -454.81 Fahrenheit). This is mostly due to a lack of atmosphere and the vacuum-like nature of space — with very few molecules to energetically bounce around, there can be no heat
c (velocity) of light in the -270.45 C
and the "new" velocity of light in the -90 C
as:
1/-90 x -270=3
or as:
1/ -270 x -90
=0,3333 of the speed of light.
The speed of light =
299 792 458 m / s
So then, 0,333 % must be equal to
299 792 460 , 99779246 km / sec
This defines the motion of light along the upper atmosphere as the change of the temperature by an amount equal to
-270.45--90
=180
as the basics of the change of the angle of the earth's atmosphere as the 180 degree constant.
So along this curvature, the light may displace into the shadow side of the earth and continue to
360 degrees.
So then the difference in temperature as the 2x 180 =360 degrees ,the multiple as shared becomes
= 90 degrees as the right angle of the shift of the day time atmosphere to the night time atmosphere.
So then the change in temperature must be related to earth's surface as the "mean temperature " = zero degrees C.
Meaning that the change in temperature may also faze to the -90 by the 180 as the change in light as related to
the x2 multiple of the speed of light in this faze change of 180 degrees as,
299 792 460 .9977 x2=599 584 741.994.
Meaning beyond the speed of light as the blue shift in this layer of the 180 degrees to the reduction into 90
degrees as the measure need for any x and y measure to have the prerequisites to make any equation with
light to be computable as physics.
here are some really suprising values of the speed of light as related to the temperature of the earth's atmospherical layers that generate
faster than light velocities.
The strange facts are that the temp change= 90 to 180 to 270 to 360.
So to does there need be some way that the temperature interacts on the basics of reentry into earth's atmosphere by being as such
90 x1c , 180 x 2c, 270 xc3 and c delta as 360
The rotation of the earth happens in space, while the rotation of any objects in reentry also rotate in space, so any temperature 1 in rotation must add to temperature 2 of the rotation and the sum being = 1+2=3
So then each new object must have the rotation as part of it's size and it is this that defines the speed of light as the larger collective of objects and their temperature as rotation variables. The speed of light has no limit. Imagine that you combine 1000 bodies in space that are larger than earth or the sun and the sum as volume related to temperature and the rate of rotation must be way much bigger than the speed of light as the x and y shows the need to compare the temp and rotation and the volume as the
C. temp . Angle. Vol >c= x / y
So then each new object must have the rotation as part of it's size and it is this that defines the speed of light as the larger collective of objects and their temperature as rotation variables. The speed of light has no limit. Imagine that you combine 1000 bodies in space that are larger than earth or the sun and the sum as volume related to temperature and the rate of rotation must be way much bigger than the speed of light as the x and y shows the need to compare the temp and rotation and the volume as the
C. temp . Angle. Vol >c= x / y
Each point along the 12345
may be extended to new functions of the "camelot" of Kennedy as the "crown functions " of the extendability to 12345-------->any number.
variables of increased light, gravity , volume, rotation , by way of the variables of every planet, star and galaxy, where each level of size
must have the ability to be observed from space at higher levels of the velocity of light.
Imagine observer outside the galaxy and imagine an observer outside the sirius star system and then imagine the observer of earth.
Each of them must be equal in the velocity of the recognitions of the amount of layers observed. So the total must equal every part of
it, and this must be faster than the speed of light.
Kennedy quote:
"Not because they are easy but because they are hard".
as related to the geometry of triangular solids and the triangular solid space created by the "hard triangles so that they create the space between them". It is this that no levitation builders ever imagined could actually lift without the use of any fuel or the use of any energy .
may be extended to new functions of the "camelot" of Kennedy as the "crown functions " of the extendability to 12345-------->any number.
variables of increased light, gravity , volume, rotation , by way of the variables of every planet, star and galaxy, where each level of size
must have the ability to be observed from space at higher levels of the velocity of light.
Imagine observer outside the galaxy and imagine an observer outside the sirius star system and then imagine the observer of earth.
Each of them must be equal in the velocity of the recognitions of the amount of layers observed. So the total must equal every part of
it, and this must be faster than the speed of light.
Kennedy quote:
"Not because they are easy but because they are hard".
as related to the geometry of triangular solids and the triangular solid space created by the "hard triangles so that they create the space between them". It is this that no levitation builders ever imagined could actually lift without the use of any fuel or the use of any energy .
Walking on the moon introduced a new angle to the inclination of the moon in reference to it being a weight application where the walkers on the moon could actually gain a levitational response by change of the body angle. Basics of making giant leaps on the moon as Kennedy's project.
This same angle of increment is the first such reference outside earth as the moon is the second body and the rules for levitation must be derived from this experience.
The leviatation occurs without any energy.
This same angle of increment is the first such reference outside earth as the moon is the second body and the rules for levitation must be derived from this experience.
The leviatation occurs without any energy.
Senator moon beam comment today:
When you continue with a line of thought, and follow it, you may actually find some things that are as far out as the ,"real x files".
When you continue with a line of thought, and follow it, you may actually find some things that are as far out as the ,"real x files".
image credit:
space.com
The top of the mesosphere, called the mesopause, is the coldest part of Earth's atmosphere, with temperatures averaging about minus 130 degrees F (minus 90 C). This layer is hard to study. Jets and balloons don't go high enough, and satellites and space shuttles orbit too high.
The dangers of reentry
A variety of Thermal Protection Systems (TPS) is employed to prevent spaceships from preemptively burning. The heat shield is a reentry vehicle's primary defense against the intense heat experienced as they fall through the atmosphere
image credit:Wikipedia
space.com
The top of the mesosphere, called the mesopause, is the coldest part of Earth's atmosphere, with temperatures averaging about minus 130 degrees F (minus 90 C). This layer is hard to study. Jets and balloons don't go high enough, and satellites and space shuttles orbit too high.
The dangers of reentry
A variety of Thermal Protection Systems (TPS) is employed to prevent spaceships from preemptively burning. The heat shield is a reentry vehicle's primary defense against the intense heat experienced as they fall through the atmosphere
image credit:Wikipedia
credit:
Wikipedia
Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet, or natural satellite. There are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris, or bolides; and controlled entry (or reentry) of a spacecraft capable of being navigated or following a predetermined course. Technologies and procedures allowing the controlled atmospheric entry, descent, and landing of spacecraft are collectively termed as EDL.
Animated illustration of different phases as a meteoroid enters the Earth's atmosphere to become visible as a meteor and land as a meteoriteAtmospheric drag and aerodynamic heating can cause atmospheric breakup capable of completely disintegrating smaller objects. These forces may cause objects with lower compressive strength to explode.
Crewed space vehicles must be slowed to subsonic speeds before parachutes or air brakes may be deployed. Such vehicles have kinetic energies typically between 50 and 1,800 megajoules, and atmospheric dissipation is the only way of expending the kinetic energy. The amount of rocket fuel required to slow the vehicle would be nearly equal to the amount used to accelerate it initially, and it is thus highly impractical to use retro rockets for the entire Earth reentry procedure. While the high temperature generated at the surface of the heat shield is due to adiabatic compression, the vehicle's kinetic energy is ultimately lost to gas friction (viscosity) after the vehicle has passed by. Other smaller energy losses include black-body radiation directly from the hot gases and chemical reactions between ionized gases.
Wikipedia
Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet, or natural satellite. There are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris, or bolides; and controlled entry (or reentry) of a spacecraft capable of being navigated or following a predetermined course. Technologies and procedures allowing the controlled atmospheric entry, descent, and landing of spacecraft are collectively termed as EDL.
Animated illustration of different phases as a meteoroid enters the Earth's atmosphere to become visible as a meteor and land as a meteoriteAtmospheric drag and aerodynamic heating can cause atmospheric breakup capable of completely disintegrating smaller objects. These forces may cause objects with lower compressive strength to explode.
Crewed space vehicles must be slowed to subsonic speeds before parachutes or air brakes may be deployed. Such vehicles have kinetic energies typically between 50 and 1,800 megajoules, and atmospheric dissipation is the only way of expending the kinetic energy. The amount of rocket fuel required to slow the vehicle would be nearly equal to the amount used to accelerate it initially, and it is thus highly impractical to use retro rockets for the entire Earth reentry procedure. While the high temperature generated at the surface of the heat shield is due to adiabatic compression, the vehicle's kinetic energy is ultimately lost to gas friction (viscosity) after the vehicle has passed by. Other smaller energy losses include black-body radiation directly from the hot gases and chemical reactions between ionized gases.