ASTR 1210 (O'Connell) Study Guide
8. GRAVITATIONAL ORBITS AND SPACE FLIGHT
Space Shuttle Discovery launches on
a mission
to the Space Station, 2001
"There will certainly be no lack of human pioneers when we have
mastered the art of [space] flight....Let us create vessels and sails adjusted
to the heavenly ether, and there will be plenty of people unafraid of
the empty wastes. In the meantime we shall prepare, for the brave
skytravelers, maps of the celestial bodies."
 Johannes Kepler (1610)

Kepler was right about the multitudes of people eager to travel into
space, but it took another 350 years of technological development to
build the "vessels" needed to carry them. Space travel is difficult.
However, the theoretical key to space flight was discovered by
Newton only 80 years after Kepler's work.
Newton's theories of dynamics and gravity provided a complete
understanding of the interaction between gravitating bodies and the
resulting orbits for planets and satellites. This guide first
describes the
nature of possible gravitational orbits
and some implications of those.
Two hundred and fifty years after he died, Newton's work became the
foundation of
space technology, which is introduced in the
second part of the guide. Space technologyrockets, the Space
Shuttle, scores of robot spacecraft, the human space programhas
provided most of our present knowledge of the Solar System and most of
the material we will discuss in the rest of this course. Commercial
space technology
(e.g.
GPS,
communications, and remote observing satellites) is already an
integral part of modern life.
The mid20th century was the first time humans had ever sent machines
beyond the Earth's atmosphere.
By 2015, we had explored every
large body in the Solar System out to the orbit of Pluto. Even
such farsighted thinkers as Galileo and Newton himself would never
have thought that possible in the mere 400 years that had elapsed
since Kepler's Laws were formulated. This was an amazing
accomplishment,
the greatest exploratory feat of humanity to
date.
A. Newtonian Orbit Theory
Orbital Dynamics
Newton's theory can accurately predict gravitational orbits
because it allows us to determine the
acceleration of an object
in a gravitational field.
Acceleration is the rate of change
of an object's velocity.
If we know the
initial position and velocity of an object, knowing its acceleration
at all later times is enough to completely determine its later path of
motion.
To predict the path, we simply substitute Newton's expression
for F_{grav} for the force term in his
Second
Law and solve for acceleration:
a = F_{grav}/m
But there are major complications. The Second Law is not a simple
algebraic expression. Both velocity and acceleration are rates of
change (of position and velocity, respectively). Mathematically,
they are derivatives. The gravitational force also changes with
position. Finally, velocity, acceleration and the gravitational force
all have a
directionality as well as a magnitude associated with
them. That is, they are "vectors".
So the Second Law is really a differential vector
equation. To solve it, Newton had to
invent
calculus.
We don't need to know the mathematical details in order to
understand the basic interaction that shapes Newtonian orbits. Take
as an example the orbit of the Earth around the Sun.
Pick any location on the Earth's orbit. Represent its velocity at that
location as an arrow (a vector) showing the direction and magnitude
of its motion.
An essential element of Newtonian theory is that changes in
the magnitude of the velocity vector (the speed) or in
the direction of motion are both considered to be
"accelerations." In the following drawings, the red arrows represent
the Earth's velocity vector and the blue arrows represent the applied
gravitational force. According to Newton's Second Law, the change
in the velocity vector (a speedup in the first case or a
deflection of the direction of motion in the second) is in the
direction of the applied force.
Starting from any location, the instantaneous velocity vector and the
rate of change of that vector (the acceleration) combine to determine
where the Earth will be at the next moment of time. Adding up the
motion from one moment to the next traces out the orbital path.
In Newtonian gravity, the gravitational force acts
radially  i.e. along the line connecting the Earth and the
Sun. Accordingly, both the
acceleration and the change in the Earth's velocity
vector from one moment in time to the next will also always be in
the radial direction.
You might think that if the acceleration is always toward the Sun,
then the Earth should fall faster and faster on a radial trajectory
until it crashes into the Sun. That's exactly what would
happen if the Earth were ever stationary in its orbit.
In that case, the situation in the left hand drawing above (straightline
acceleration toward the Sun) would prevail.
But if the Earth's velocity vector has a component which is perpendicular
to the radial direction, then in any interval in time, it will move
"sideways" at the same time as it accelerates toward the Sun.
If the combination of sideways motion and distance from the Sun is
correct, the Earth will avoid collision with the Sun, and it will
stay in permanent orbit. The animation at the right shows the
situation for the Earth's (exaggerated) elliptical orbit around the
Sun (here, the blue line is the velocity vector, the green line is the
acceleration;
click for an
enlargement). Note that where
the Earth is nearest the Sun, the gravitational force and inward acceleration
are greatest, but the sideways motion is also greatest, which prevents us
from colliding with the Sun. That motion is in accordance with
Kepler's
second law.
Therefore, all permanently orbiting bodies are perpetually
falling toward the source of gravity but have enough sideways
motion to avoid a collision.
Kinds of Gravitational Orbits
In the case of two gravitating objects (for example, the Earth and the
Moon, the Sun and a planet, or the Earth and an artificial satellite),
Newton found that the full solutions of his equations give the
following results:
 The relative orbit is confined to a geometric plane which
contains both objects.
 The shape of the orbit within the plane is a "conic section",
of which there are only four types.
 A circle
 An ellipse
 A parabola
 A hyperbola
See the illustration at the right.
 The orbital type is determined by the
initial distance, speed (V) and
direction of motion of the orbiting object, as follows:
 Define the "escape velocity" at a given
distance: V_{esc}(R) = √(2GM/R), where R
is the separation between the two objects and M is
the mass of the primary object.
V_{esc} for the Earth at the Earth's surface is 25,000 mph (or 11 km/s).
V_{esc} for the Sun at the Earth's 1 AU distance from the Sun
is 94,000 mph (42 km/s).
 If V < V_{esc}, the orbit is an ellipse
or circle. It is said to be "closed" or
"bound". The smaller object will permanently
repeat its orbital motion.
 If V ≥ V_{esc}, the orbit is a parabola or
hyperbola. It is said to be "open" or "unbound".
The smaller object escapes and does not return.
 Only specific values of velocity will yield circular or
parabolic
orbits. An object moving exactly at escape velocity will move on a
parabola. To achieve a circular orbit an object must move at 71% of
the escape velocity, and its velocity must be exactly
perpendicular to the radial direction. Other combinations of
velocity or direction lead to elliptical or hyperbolic orbits.
 As noted earlier, shapes and motions within the "closed" orbits
for the planets satisfy all three of Kepler's Laws of planetary
motion.
You can interactively explore the relation between the orbit and the
initial velocity vector using the Flash animation
Gravity Chaos.
Newton's Mountain
Newton illustrated orbital behavior for a simple idealized situation
where a powerful cannon is fixed in position on top of a high mountain
on the Earth's equator. It is allowed to fire only with its barrel
parallel to the Earth's surface (see the illustration below). Since
both the distance from Earth's center and the direction of initial
flight are fixed, the cannonball follows an orbit that depends
only
on the muzzle velocity of the cannon as shown below.
The gravitational force of a spherical body like the Earth acts as
though it originates from the center of the sphere, so
elliptical orbits of the cannonball will have the center of the Earth
at one focus. The center of the Earth lies directly under the red
dot in the picture below.
(For simplicity, the diagram omits showing "orbits" where the muzzle
velocity is far enough below the circular orbit velocity that the
cannonball hits the surface of the Earth. Needless to say, that is
the situation for all reallife cannons; but the flight paths taken
before the collision do have elliptical shapes.)
"Newton's Mountain": orbit type depends on
initial velocity.
From lower to higher velocities, orbit shapes are:
ellipse, circle, ellipse, parabola, hyperbola.
"Escape velocity" (which
is 25,000 mph at Earth's surface) produces
a parabolic orbit.
General Relativity
Much later (1915), Newton's theory was shown by Albert
Einstein
to be inadequate in the presence of large masses or over large
distances and has been replaced by
the
General
Theory of Relativity in such situations. Relativity
theory
profoundly changed our understanding of space and time,
for example by demonstrating that mass and energy can affect the
structure of space and time, something that Newton never contemplated.
It is much more complicated mathematically than Newton's formulation.
But as a practical matter,
Newton's theory is an entirely
satisfactory description of "everyday" gravity. Only very minor
corrections to the Newtonian predictions are necessary, for example,
to send spacecraft with high accuracy throughout the solar
system.
General Relativity predicted important phenomena that were not foreseen in
Newtonian physics,
including black
holes (closed regions of spacetime around massive, compact
objects)
and
gravitational waves (propagating disturbances in the structure of
spacetime).
The first detection of cosmic gravitational waves, generated by the
merger of two very distant black holes, was announced by
LIGO (the Laser
Interferometer GravitationalWave Observatory) in February of 2016.
This was one of the most difficult scientific experiments ever
attempted as well as a brilliant confirmation of the validity
of General Relativity.
B. Important Implications of Newtonian Orbits
"FreeFall" Orbits
Free motion in response to gravity (in the absence of other forces) is
called "freefall" motion. Conic section
orbits are all "freefall orbits."
Remember that motion is normal in freefall. For instance,
rocket engines do not have to be on in order for spacecraft to
move through space on a freefall orbit. Spacecraft will "coast" forever on
such an orbit, just as do the planets in orbit around the Sun.
Note also that freefall orbits will depart from simple conic
sections if an object is under the influence of
more than one gravitating body. For instance, comets
are often deflected from their Sundominated simple conic orbits by
Jupiter's gravity (see Guide 21),
and spacecraft traveling between the Earth and the Moon will not
follow simple conic paths.
Freefall orbits are independent of the mass of the orbiting object.
Another way of stating this is to say that the acceleration of all
objects is the same in a given gravity field (e.g. at a given
distance from the Sun or near the Earth's surface), regardless of
their masses. This was first demonstrated experimentally
by Galileo
and was the subject of our "object drop" Puzzlah (see
Study Guide 7).
The mass of the orbiting body always
cancels out of the expression for acceleration under gravity.
For instance, in the case of a planet orbiting the Sun, the
gravitational force on the planet is directly proportional to
the planet's mass; but, according to Newton's Second Law, the resulting
acceleration is inversely proportional to its mass. So,
mass drops out of the expression for acceleration.
This is true for all orbits under gravity. Hence, a tennis ball in
space, if it were moving with the same speed and direction as the
Earth at any point, would follow exactly the same orbital path as the
Earth around the Sun.
Kepler's Third Law (that the orbital period of a planet around the Sun
depends only on its orbital size, not on the mass of the planet) is another
manifestation of this fact.
A more familiar manifestation of "free fall" these days is the
phenomenon of "floating" astronauts on space missions. Even
though the spacecraft is much more massive, both the astronauts
and the spacecraft have identical accelerations under the
external gravitational fields. They are moving on parallel
freefall orbits, so the astronauts appear to be floating and
stationary with respect to the spacecraft, even though they are
actually both moving at over ten thousand miles per hour in
nearEarth orbit.
Turning on a rocket engine breaks its freefall path. Rocket
engines are described under (C) below. You can think of a rocket
engine in the abstract as a device for
changing from one freefall orbit to another by applying a
nongravitational force.
With its engine turned off, the motion of any
spacecraft is a freefall orbit.
If the engine is on, the craft is
not in free fall. For instance, the orbit of the Space Shuttle
launching from the Earth will depart from a conic section until its
engines turn off. An example of using a rocket engine to change from
one freefall orbit to another
is shown here.
The Russian "Mir" space station (19862001) orbiting
Earth in freefall at an altitude of 200 miles with a velocity of 17,000
mph
Geosynchronous Orbits
According to Kepler's Third Law, the
orbital period of a satellite will
increase as its orbital size increases. We have exploited that
fact in developing one of the most important practical
applications of space technology: geosynchronous satellites.
 Spacecraft in "low" Earth orbits (less than about 500 mi),
like the Mir space station (seen above) or the Space Shuttle, all
orbit Earth in about 90 minutes, at 17,000 miles per hour,
regardless of their mass. As seen from a given point on Earth's
surface, they travel quickly across the sky and never spend more
than about 10 minutes above the local horizon.
 However, the orbital period of a spacecraft in a
larger orbit will be longer. For an orbit of radius
about 26,000 mi, the period will be 24 hoursthe same
as the rotation period of the Earth. Spacecraft here, if they are
moving in the right direction, will appear to "hover"
permanently over a given point on the Earth's surface. These orbits
are therefore called geosynchronous or
"geostationary." See the animation above. This is the ideal location
for placing communications satellites.
[The concept of geosynchronous communications satellites was first
proposed by science fiction
writer Arthur
C. Clarke. He deliberately did not patent his idea, which became
the basis of a trilliondollar industry.]
Applications of Kepler's Third Law
Newton's theory verified Kepler's
Third Law (described in Guide 7) and provided a physical
interpretation of it. Newton found, as did Kepler, that for the
planets in the Solar System, P^{2} = K a^{3},
where P is the period of a planet in its orbit, a is
the semimajor axis of the orbit, and K is a constant. But his
gravitational theory allowed him to show that the value of K is K =
4π^{2}/GM, where M is the mass of the Sun.
More generally, K is inversely proportional to the mass of the
primary body (i.e. the Sun in the case of the planetary orbits but
the Earth in the case of orbiting spacecraft). The larger the
mass of the primary, the shorter the period for a given
orbital size.
 The Third Law therefore has an invaluable astrophysical
application: once the value of the "G" constant has been determined
(in the laboratory), the motions of orbiting objects can be used to
determine the mass of the primary. This is true no matter how far
from us the objects are (as long as the orbital motion and size can be
measured).
 In the Solar System, the Third Law allows us to determine the
mass of the Sun from the size and periods of the planetary orbits.
It allows us to determine the mass of other planets from the
orbits of their satellites. In the case of Jupiter, for example, the
periods and sizes of the orbits of the Galilean satellites can be used
to determine Jupiter's mass, as
in Optional Lab 3.
Remember that freefall orbits are independent
of the mass of the orbiting body. This means that the mass of a given
planet cannot be determined from its motion or orbital size
around the Sun.
 The Third Law was critical in determining the masses of other
stars, using their orbits in binary star systems, and hence to
deducing the physical processes that
control
stellar structure and evolution, one of the great accomplishments
of 20thcentury physics.
 The Third Law is applied today to such diverse astronomical
problems as measuring the masses of "exoplanets" around other
stars (see Study Guide 11) and establishing
the existence of "Dark Matter" in distant galaxies.
Schematic diagram of a liquidfueled rocket engine.
Rockets carry both fuel and an oxidizer,
which allows the fuel to burn
even in the absence of an oxygenrich atmosphere.
The thrust of the
engine is proportional to the velocity of the exhaust gases
(V_{e}).
C. Space Flight
If the primary technology enabling space flight is Newtonian
orbit theory, the second most important technology is the
rocket engine.
 In a rocket engine such as that shown in the diagram above, fuel
combined with oxidizer is burned rapidly in a combustion chamber and
converted into a large quantity of hot gas. The gas creates high
pressure, which causes it to be expelled out a nozzle at very high
velocity.
The exhaust pressure
simultaneously forces the body of the rocket forward. You can think
of the rocket as "pushing off" from the moving molecules of exhaust
gas. The higher the exhaust velocity, the higher the thrust.
Note: rockets do not "push off" against the air or against the
Earth's surface. Rather, it is the "reaction force" between the
expelled exhaust and the rocket itself that impells the rocket forward.
Designers work to achieve the highest possible exhaust velocity per
gram of fuel. Newton's second law of motion and various elaborations
of it are essential for understanding and designing rocket motors.
[Rockets always carry their own supply of oxidizer (as seen in the
diagram above). This distinguishes them from ordinary aircraft
engines (propeller or "jet"), which use oxygen from the Earth's
atmosphere as an oxidizer. Obviously, there aren't any handy
oxidizers available in the vacuum of space.]
 The main challenge to spaceflight is obtaining the power needed to
reach escape velocity. For Earth, this is 11 km/sec
or 25,000 mph.
The first successful launch of a
spacecraft, the
USSR's Sputnik1, reached only 18,000 mph, but that was sufficient to
place this "artificial satellite" into an elliptical orbit around
Earth at several hundred miles altitude.
Modern "standard" rocket engines are designed for launching commercial
payloads to synchronous orbit or delivering intercontinental ballistic
misslesneither of which involve reaching escape velocity from
Earth. Therefore, most scientific spacecraft for planetary missions
are relatively small (i.e. low mass) in order that standard engines
can propel them past Earth escape velocity. This means that many
clever strategies are needed to pack high performance into small,
light packages.
Example: The New Horizons
spacecraft, launched on a superhigh velocity trajectory to Pluto in
2006, has a mass of only 1050 lbs; its launching rocket weighed
1,260,000 lbs, over 1000 times more! New Horizons flew past
Pluto in July 2015, traveling at over 34,000 mph, and has delivered a
treasuretrove of images and other data on this most distant (3
billion miles from Earth at the encounter) of the classical
planets.
A rocket launched at exactly escape velocity from a given parent body
will eventually, at very large distances, slow to exactly zero
velocity with respect to that body (ignoring the effect of other
gravitating bodies).
The Apollo program used the extremely
powerful Saturn V rockets to
launch payloads with masses up to 100,000 pounds (including 3 crew
members) to the Moon. This technology was, however, retired in the
mid1970's because it was thought, erroneously, that the next
generation of "reusable" Space Shuttle vehicles would be cheaper to
operate. A big mistake, because the reusable parts required
extensive (and expensive) refurbishing for each new flight.
The Space Shuttle (shown above) was fueled by high energy
liquid oxygen and liquid hydrogen plus solidrocket boosters. But it
was so massive compared to the power of its engines that it
could not reach escape velocity from Earth. Its maximum
altitude is only about 300 miles. That is why NASA and the private
sector are
developing new
"heavy lift" rocket technologies which have replaced the Shuttle,
the most successful to date being
the SpaceX Falcon and Dragon
spacecraft.
Modern rocket engines are remarkably
complicated. Here
is a simplified schematic of the Space Shuttle main engines.
D. Interplanetary Space Missions
Beginning in the early 1960's, NASA and
foreign space agencies developed a series of evermore sophisticated
robot probes to study the Sun, Moon, planets, and the
interplanetary medium. These included
flyby spacecraft,
orbiters, landers, rovers, and samplereturn vehicles.
As of 2015, only 58 years after the first successful satellite launch
(Sputnik, in 1957), we had flown at close range past every planet
including Pluto; had placed robotic observatories into orbit around
the Moon, Mercury, Venus, Mars, Jupiter, Saturn, three asteroids, and
one comet; had sent probes into a comet nucleus and the atmosphere of
Jupiter; had softlanded on the Moon, Venus, Mars, Saturn's moon
Titan, and the comet ChuryumovGerasimenko; and had returned to Earth
samples obtained from the coma of the comet Wild 2 and from a
softlanding on the asteroid Itokawa. And in 2013, the first human
spacecraft left the Solar System altogether and entered interstellar
space. At right is an artist's concept painting of the Cassini
mission in orbit around Saturn.
We also put a number of highly capable
remotecontrolled
observatories for studying the Solar System and the distant
universe (such as the Hubble Space Telescope, the Chandra XRay
Observatory, and the James Webb Space Telescope) into orbit around the
Earth and the Sun.
Of course, the Apollo program in the 1960's
also
sent human beings to the Moon.
But, by far,
most of what we know about the denizens of the
Solar System has come from our powerful
robot missions and
observatories, most of which were not even in development by the
end of the Apollo program in 1972.
For a list of these missions and additional
links,
click here.
For a nice, prospective view of what
human expansion over the next
couple centuries into the deep space of our Solar System might
look like, see this
video,
based on Carl Sagan's writings.
E. The Cost of Space Missions
Ever wonder why space flight is so expensive? It's
because
thousands of people are involved in almost any space
endeavor, and it takes anywhere from
5 to 30 years to prepare a
space mission.
Spacecraft require not only their own launching and maneuvering
engines but also command and control systems, power supplies, thermal
control, pointing and stabilization systems, protection from a harsh
environment, sensors and scientific instruments, data taking and
storage systems, communications systems, and more  all of these
subject to stringent weight and volume constraints  plus extensive
Earthbased infrastructure to monitor and operate them. All those
people are required in order to design and build these myriad
components and then certify that they will be at least 95% reliable
after launch  because, with very few exceptions, no repair is
possible. They must identify and mitigate all possible failure
modes.
Reliability is the principal cost driver of space
missions. Needless to say, because of the demands of human safety,
the cost of crewed missions greatly exceeds that of comparablyscaled
robot missions.
Two examples:
 Wikipedia reports that "The
Gemini 9A
mission (a 1966, 3day, low Earth orbit test flight with two astronauts)
was supported by 11,301 personnel, 92 aircraft and 15 ships from the
U.S. Department of Defense"  not to mention thousands of NASA and
private sector personnel.
 The Apollo Moon program
involved a total of 410,000 people and 20,000 companies. Its $150
billion budget (in 2019 dollars) supported about 1,200,000
personyears of effort over 10 elapsed years  the largest
nonmilitary project in history. For a modern overview of the scope
and complexity of the Apollo program, see the recent book
"One
Giant Leap" by Charles Fishman. NASA's overall budget
history is shown here. At its
peak, the Apollo program accounted for over 4% of the total US federal
budget.
The overall unique scientific, commercial or exploratory value of a
space mission must be weighed carefully against its projected
cost.
To get a feel for the scale of effort involved in preparing and
launching major spacecraft, watch this:
The Hubble Space Telescope on orbit 300 miles above Earth
Reading for this lecture:
Bennett textbook: Ch. 4.14.4 (Newtonian dynamics &
gravitational orbits)
Study Guide 8
Reading for next lecture:
Study Guide 9 (this material is not covered in the text)
Web links:
Last modified
September 2023 by rwo
Text copyright © 19982023 Robert W. O'Connell. All
rights reserved. Orbital animation copyright © Jim Swift,
Northern Arizona University. Conic section drawings from ASTR
161, University of Tennessee at Knoxville. Newton's Mountain
drawing copyright © Brooks/ColeThomson. These notes are
intended for the private, noncommercial use of students enrolled
in Astronomy 1210 at the University of Virginia.