This is only a preview of the September 1997 issue of Silicon Chip. You can view 29 of the 96 pages in the full issue, including the advertisments. For full access, purchase the issue for $10.00 or subscribe for access to the latest issues. Items relevant to "Multi-Spark Capacitor Discharge Ignition System":
Items relevant to "Building The 500W Audio Power Amplifier; Pt.2":
Articles in this series:
Items relevant to "PC Card For Controlling Two Stepper Motors":
|
By SAMMY ISREB
Picture credit: NASA/JPL
The Cassini space
probe: unravelling
Saturn’s secrets
Following its spectacularly successful Mars landing,
NASA is readying a spacecraft to probe Saturn and its
moons. The Cassini probe, as it is known, should
provide new insights into the solar system.
4 Silicon Chip
Picture credit: NASA/JPL
O
N OCTOBER 6TH this year,
NASA and JPL (Jet Propulsion
Laboratories) will launch their
latest space probe, the Cassini, using a
Titan IV rocket. This launch will herald the start of an almost decade-long
mission designed to explore Saturn
and its moons.
Many aspects of this mission are
ground breaking, as we shall see. And
as with other space probes, the Deep
Space Network site at Tidbinbilla
near Canberra will be involved in the
mission.
Saturn Orbit Insertion: this is a computer-rendered image of Cassini during the
Saturn Orbit Insertion (SOI) manoeuvre, just after the main engine has begun
firing. The SOI manoeuvre, approximately 90 minutes long, will allow Cassini
to be pulled by Saturn’s gravity into a 5-month orbit. Cassini’s close proximity to
the planet after the manoeuvre will offer an opportunity to observe Saturn and
its rings at high resolution.
The launch
The Titan IV rocket that will be
used to launch the Cassini probe is
immense, with a prelaunch weight
of 940,000kg, of which 840,000kg is
propellant. But despite the power of
the Titan IV rocket, its launch energy is not enough to send the almost
5.5-tonne space probe directly on
its way. To overcome this, the probe
will first be sent towards Venus and
will then use the gravitational field of
this and other planets to accelerate it
towards Saturn.
Initially, the Cassini probe and Centaur upper stage of the rocket will be
placed in an Earth orbit. This “stack”
Cassini Interplanetary Trajectory: this graphic depicts the planned inter
planetary flight path beginning with the launch from Earth on 6th October 1997,
followed by gravity assisted flybys of Venus (21st April 1998 and 20th June
1999) and Jupiter (30th December 2000). The Saturn arrival is scheduled for 1st
July 2004, which marks the beginning of a 4-year tour of the Saturn system.
September 1997 5
Table1: Cassini Probe Mission Events
Mission Event
Date
Launch on Titan IV launch vehicle
6th October, 1997
Aphelion 1 (furthest distance from the Sun
1st November, 1997
Perihelion 1 (closest approach to Sun)
23rd March, 1998
Venus 1 flyby
21st April, 1998
Deep space manoeuvre to target Venus 2
2nd December, 1998
Aphelion 2 (furthest distance from the Sun
4th December, 1998
Window for using high gain antenna begins
16th December 1998
Window for using high gain antenna ends
10th January, 1999
Venus 2 flyby
20th June, 1999
Perihelion 2 (closest approach to Sun)
27th June, 1999
Earth flyby
16th August, 1999
High gain antenna can be used from now on
29th January, 2000
Jupiter flyby
30th December, 2000
Science observations begin
1st January, 2004
Saturn orbit insertion manoeuvre
1st July, 2004
Manoeuvre to target probe on Titan
12th September, 2004
Huygens probe separates from Cassini to go to Titan
6th November, 2004
Manoeuvre to target for Titan flyby
8th November, 2004
Huygens probe mission at Titan (approx, 4 hours long)
27th November, 2004
First flyby of Titan, Saturn's largest moon
27th November, 2004
Nominal end of mission (after 11 years)
1st July, 2008
End of possible extended mission
Unknown
will orbit the Earth unpowered for
about 15 minutes until it is in line
with Venus, at which stage the powerful Centaur stage will be ignited to
provide the final push towards Venus
and to enable the probe to escape the
Earth’s gravitational field.
At the end of its 8-minute burn, the
Centaur stage will separate from Cassini. However, before this occurs, the
various subsystems in the spacecraft
will be activated so that it can operate
on its own. As well as this, before separation, the Centaur’s computer will
point the Cassini’s high gain antenna
towards the Sun. This is done so that
the antenna shields the instruments
and the avionics from the intense
heat of the Sun as the spacecraft approaches Venus.
Following separation, communication with the spacecraft will be made
6 Silicon Chip
through the 34-metre antenna at the
Deep Space Network at Tidbinbilla.
This will enable ground controllers
at the Jet Propulsion Laboratories to
monitor the status of the probe and to
send commands to prepare it for its
long journey to Saturn.
Gravity assist
As already mentioned, the Cassini
probe is not able to make it directly
to Saturn. This problem is overcome
by using a “gravity assist” technique
four times during the flight: at Venus
in April 1998 and again in June 1999;
at Earth in August 1999; and at Jupiter in December 2000. During a brief
period between the Venus encounters
and shortly after the Earth flyby, the
heat radiation from the Sun will be
low enough to allow the antenna to
be pointed towards Earth. This will
improve communications with the
spacecraft and assist in its navigation.
As well as using the gravity assists,
the Cassini space probe will also
use two types of fuels to get to its
destination. The first of these fuels is
known as “bipropellant” and is used
for large course alterations. Bipropellant is made up of two chemicals,
mono-methyl-hydrazine and nitrogen
tetraoxide, which ignite when combined in the engine nozzles. These
two chemicals are easy to store and,
importantly, they do not freeze at the
low temperatures that will be experienced on the mission.
The second fuel used is hydrazine.
This powers the “Reaction Control
Thrusters” and will be used for very
brief burns to alter the rotational position of the Cassini. The hydrazine
will only be used in small amounts
and engineers are confident that about
half the original quantity will remain
at the end of the planned mission.
The main objective of the navigators
at JPL is to keep the spacecraft to the
planned trajectory for the entire mission. The navigation team provides
the project with predictions of the
trajectory of the Cassini probe, the
various planets, and Saturn’s satellites. Based on this information, the
team then determines the trajectory
correction manoeuvres (TCMs) that
are re
quired to maintain the preplanned trajectory. Without these
many small corrections, the spacecraft
would miss Saturn by many millions
of kilometres.
Tracking techniques
In order to plan for TCMs, the
navigators use a number of different
techniques to track the spacecraft’s
trajectory and determine its position. The three methods used are: (1)
Doppler, (2) ranging, and (3) optical
navigation.
The Doppler technique is used to
measure the speed that the Cassini
is approaching or receding from the
Earth and is similar to the Doppler
technique used in radar speed guns.
Basically, the Deep Space Network
antenna sends a signal to the spacecraft which is then directly returned.
If the spacecraft is approaching or
receding from the tracking station, the
frequency of the return signal will by
slightly higher or lower, respectively.
This frequency difference allows the
spacecraft’s velocity to be determined
ABOVE: Huygens Probe Release –
artist’s conception of Cassini orbiter
with the Huygens probe separating
to enter Titan’s atmosphere. After
separation, the probe will drift for
about three weeks until it reaches its
destination. Equipped with a variety
of scientific sensors, the ESA Huygens
probe will spend 2-2.5 hours
descending through Titan’s dense
murky atmosphere of nitrogen and
carbon-based molecules, beaming its
findings to the distant Cassini orbiter
as it flies overhead.
Picture credit: NASA/JPL
Picture credit: NASA/JPL
RIGHT: Huygens Probe Exploded
View – the probe has a diameter of 2.7
metres and a mass of nearly 350kg.
It contains a heat shield, parachute
package, engineering equipment
including batteries, and several
scientific sensors to measure the
properties of Titan’s atmosphere and
surface.
September 1997 7
successive encounters. The first takes
place just after the encounter and is
designed to correct any errors in the
trajectory. The second and third TCMs
are essentially course corrections on
the way to the next encounter.
In addition to these manoeuvres,
there is a large deep space manoeuvre
between the two Venus encounters.
An additional propulsive correction
manoeuvre is also needed before and
after the Jupiter encounters.
During the Saturn approach, the
optical cameras will be calibrated so
that images of Saturn’s satellites can
be obtained. A flypast of Phoebe, Saturn’s most distant satellite, will occur
some 19 days prior to the spacecraft’s
arrival at Saturn itself.
Communications
Picture credit: NASA/JPL
Huygens Descent Profile: this picture illustrates the Huygens probe descent
profile, beginning with the initial encounter with the Titan atmosphere and
subsequent deceleration. As the probe slows, a small parachute is released
which deploys the main probe parachute. Once the parachute is fully open, the
deceleration shield is jettisoned and the probe drifts towards Titan’s surface.
About 40km above the surface the main parachute is jettisoned and a smaller
drogue chute carries the probe the remaining distance.
and therefore indicates where the
probe is headed.
Ranging operates on the principle
that radio waves travel at the speed
of light. Knowing this, navigators can
“fire” radio waves at the Cassini probe
and measure the time it takes for them
to return. The distance of the probe
from Earth can then be calculated.
When combined with the Doppler
method, this allows the spacecraft’s
position and speed to be determined
very accurately.
The optical data consists of pictures
of celestial bodies against a star background, as taken with the spacecraft’s
8 Silicon Chip
cameras. The measurements extracted
from these pictures can then be used
to determine where the spacecraft is
with respect to everything else in the
field of view. In many cases, however, optical data is used to determine
where the celestial body is rather
than the position of the spacecraft.
This will especially apply to some
of the satellites of Saturn that have
unknown orbits.
During the early part of the cruise to
Saturn, the focus of the navigational
team will be on successful planetary
flybys. The TCMs required typically
involve three manoeuvres between
The Cassini craft communicates via
a 4-metre high gain antenna, along
with two wide-beam low-gain antennas. The craft transmits to Earth at a
frequency of about 8.4GHz, while the
Earth base stations respond at about
7.2GHz. The radio link provides data
transmission rates that vary from a low
40 bits per second, right up to 170,000
bits per second. The signals will take
around an hour to reach the Earth from
Saturn and vice versa!
Back on Earth, the three stations
that make up the Deep Space Network, will be used to communicate
with the spacecraft. This network
consists of three sites spaced around
the world: (1) Tidbinbilla, Australia;
(2) Goldstone, California (USA); and
(3) Madrid, Spain.
Before any important data is sent
from Cassini, it is first placed into
one of two solid state recorders carried aboard the craft. These solid
state recorders each have a storage
capacity of two gigabits. When enough
data has been accumulated and the
right conditions prevail, an inbuilt
processor (called the Command and
Data Subsystem) will transmit the
information to Earth.
Releasing the probe
An important part of the Cassini
spacecraft is the Huygens probe,
which was supplied by the European Space Agency. This probe carries
a well-equipped robotic laboratory
which will be used to scrutinize the
clouds, atmosphere and surface of Saturn’s moon Titan. It will be released
by Cassini in November 2004 and will
LEFT: The Saturn System – this
montage of images of the Saturnian
system was prepared from an
assemblage of images taken by the
Voyager 1 spacecraft during its Saturn
encounter in November 1980. This
artist’s arrangement shows Dione in
the forefront, Saturn rising behind,
Tethys and Mimas fading in the
distance to the right, Enceladus and
Rhea of Saturn’s rings to the left and
Titan in its distant orbit at the top.
BELOW: Cassini Spacecraft (with
Huygens Probe attached) – roughly
two storeys tall and weighing more
than 5.5 tonnes, Cassini is one of the
largest interplanetary spacecraft ever
launched. Three separate antennas –
one high gain and two low gain – will
enable the orbiter to communicate
with Earth. Propulsion for large
changes to the orbiter’s trajectory
is provided by two powerful 445-N
engines. Sixteen smaller thrusters will
serve to control Cassini’s orientation
in space and make small changes to
the spacecraft’s flight path.
Picture credit: NASA/JPL
drop into Titan’s atmosphere several
weeks later.
After releasing the probe, the Cassini spacecraft will perform a manoeuvre so that it will be above the
probe when it arrives at Titan. This
will allow the spacecraft to monitor
data transmissions from the probe as
it approaches Titan’s surface. As before, the received data will be stored
in the orbiter’s solid state recorder
before being downloaded to one of
the Earth stations.
As the probe enters Titan’s upper
atmosphere it initially uses a heat
shield to decelerate. Subsequently,
at an altitude of about 175km, the
probe deploys its main parachute,
jettisons the heatshield and begins its
experiments. Fifteen minutes later, it
jettisons the main chute, deploys a
smaller parachute, and descends the
last 140km or so to the surface, collecting data all the way and transmitting
it back to the spacecraft.
As the Huygens probe breaks
through the clouds of Titan, an onboard camera will capture pictures
of the Titan panorama. Other instruments will directly measure the organic chemistry in Titan’s atmosphere and
remotely measure the composition of
the surface.
Once the mission has been completed, the spacecraft will aim its
Picture credit: NASA/JPL
antenna towards Earth and transmit
the recorded probe data. This data
will actually be transmitted twice and
will be verified on the ground before
it is overwritten in the data recorders.
After the Huygens probe has completed its mission, the space probe
will set about tackling various other
scientific missions. The spacecraft carries a number of instruments and the
main units and their scientific aims
are listed in the accompanying panel.
The planned mission will finish in
2008, after spending about four years
at Saturn and its moons. By then, the
Cassini probe will have collected huge
amounts of data over its 11-year mission lifetime and will have provided
new insights into Saturn and other
SC
parts of the solar system.
September 1997 9
|