4.16.3 EARTH
SATELITE MOVEMENT
Background and actual explanation
Every cosmic body has a gravitational field that extends out indefinitely, and theoretically, any observer is always under the simultaneous gravitational effect of all cosmic bodies. From these influences, an Earth observer, notice only the gravitational effect of closed cosmic body, Earth, Moon, Sun, other planets of Solar System.
For an observer
which distances from Earth, a decreasing of its attractive force will be
measuread, simultaneously with the increasing effect of other heavenly bodies. There
is a point where the equilibrium of these forces is attaint.
This point is the most unsecure place in a real word, because the distance between the cosmical body does not remain constant in time. Due to the continuos modification of distance between the celestial bodies, the equilibrium of force for a body situated in the free gravitational efect point is perturbed and the observer will fall in the direction of one celestial body.
In
order to attain a secure, stable state of weightlessness, it is accepted that
it is possible to escape the effect of gravity in the second way: with the aid
of inertial forces. In case of a circular free orbiting of an object around the
Earth, the object's weight is offset by the centrifugal force generated during
the orbiting. The object is, therefore, in a stable state of free suspension in
relation to the Earth.
Von Braun explained,
quite long time ago, using the mental experiment of
Acting on the satellite,
according to his description, are two forces: gravity, pulling the satellite
toward Earth, and centrifugal force, pushing the satellite away.
Von Braun quotations: as the object is moving faster speed its
trajectory will be less deflected because the centrifugal force is increased by
its higher speed, and more effectively counteracts the Earth's gravitational
pull”; and "A
circular orbit occurs whenever a small mass, travelling through the
gravitational field of a big one, happens to have a speed at which the
centrifugal force is precisely strong enough to balance the large body's
gravitational pull." [...] If the balance between gravitational and
centrifugal force is not perfect, [...] the small body will describe an
elliptical path around the large one."
Proposed explanation
If a gravitational field
is equivalent with a accelerated field, in order to put a satelite on the orbit
a very simple problem should be solved; at a certain distance d from Earth, as
example, the satelite should have a opposite acceleration, able to compensate
the attraction of Earth like in fig 1 . Because, the
gravitational acceleration is directed to the center of Earth considered like a
sphere, it is very simple to determine the direction of compensating
accelerated field.

Figure 1.
Acceleration compensation
In practice, in order to
place a body on a Earth orbit, the body is accelerated
tangential to the direction of gravitational acceleration. As consequence,
related to the center of force (Earth) a centripetal acceleration is counted. This
means, over satelite act two forces, one is gravitational acceleration and
second is a centripete forces generated using propelant during satelite
placement on the orbit or after that with the occasion of periodic corrections
of satellite position.
The centripetal component
can be very easy put under another form
, but there is
so:
![]()
The form of centripetal
force is similar with the field of a vortex (dependence related to the cube of
distance), and practically the satelite is moving under the field of a
gravitovortex force as was already presented in gravitation book and the total
force acting over him is:
![]()
It is important to
emphasize that both forces are real and every of them produce distinct effects.
It is not possible to identify the newtonian atraction force as being equal
with centripetal (or centrifugal ) force.

Figure 2. Total
force acting over a sattelite
How is repected the
third
The newtonian
component makes the satelite to fall in the gravitational field of Earth and
also the Earth to fall in gravitational field of sattelite. Due to the mass
differences, anyone counts only the falling of sattelite in Earth gravitational
field.
The centripetal
component is generated using propelant and aplying the momentum conservation
low there is a dependence between rotational motion of
satelite and quantity and direction of ejected gases.
For every observer both
forces are real and in real word the pseudoforces are inexistents.
In order to count the
real movement of an object, an accelerated observer (like an Earth observer),
as was described in chapter II, should remove first the proper movements on
order to get the real motion of studied object.
As example, for a
stationary satellite related to an Earth observer, it is wrong to consider the
satellite acted only by gravitational force. Because the Earth observer is
rotating with the same centripetal acceleration like stationary sattelite, for
him it is impposible to see the effects of this accelerations.
The equality of gravitational force with a centripet or ,,centrifugal
force” is out of question. If two forces are equal and opposite, the movement
of a body is a linear one with constant speed. Nothing is more absurd in actual
physics that considering the equilibrium of two forces lead to a stable
rotational motion.
If the Earth observer firstly
removes its proper motion, he will count the real movement of satellite and
besides the newtonian atracation also a centripetal
force will be observed.
It is wrong to consider
a satellite falling, just as an apple does when pulled down by gravity. If the
satellite wouldn’t be tangentially accelerated using propelant, in this case
there it will be a similitude between falling apple and falling satelite and
both movements are linear.
The low of physics must
represent the reality of phenomena and not the subjective perception of a
subject. It is impposible to be admited the fact that an observer who does not
count a force, it means that force does not exist.