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Galileo
Jupiter orbiter and atmospheric probe
Launch: 18 October 1989
Jupiter Arrival: 7 December 1995
Galileo Europa Mission
December 7, 1997-December 31, 1999
8 Europa encounters
December 16, 1997 - Feb 1, 1999
Perijove reduction/water/Io Torus study
May 5, 1999 - Sept 16, 1999
Io approaches
Oct 11, 1999 and Nov 26, 1999
End of mission: Dec 31, 1999
Galileo Home Page
Galileo Jupiter Orbit Tour
Jun 96 - Nov 97
Galileo Europa Mission (GEM)
Galileo Europa Mission (GEM) Fact Sheet
Where's Galileo Right Now?
COUNTDOWN
Next Galileo Spacecraft Satellite Encounters:
"Europa 13" - February 10, 1998
13 February 1998 - Gregory A. Smith
Europa - Ice Rafting
The
full data sets from Galileo's first three orbits (G1, G2 & E3)
are now validated and available!
The
Galileo Europa Mission
, an extension of the primary mission, is well on its way. The Galileo
spacecraft successfully completed its second encounter of its extended
mission with
Jupiter's moon,
Europa, on February 10, 1998.
The first Europa encounter of the extended mission occured on December 16, 1997,
when the Galileo spacecraft made the closest ever flyby of Europa.
The
Galileo Europa Mission
will include 7 more consecutive flybys of
Europa
The Galileo Europa encounters schedule:
E12 Europa - 16 December 1997
E13 Europa - 10 February 1998
E14 Europa - 29 March 1998
E15 Europa - 31 May 1998
E16 Europa - 21 July 1998
E17 Europa - 26 September 1998
E18 Europa - 22 November 1998
E19 Europa - 1 February 1999
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Mars Global Surveyor
Mars orbiter
Launch: 7 Nov 1996
Arrival: 12 Sep 1997
Mars Global Surveyor Home Page
Mars Global Surveyor (NSSDC)
Current Flight Status Report
Upcoming Mission Events
JPL Mars Missions Mirror Sites
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13 February 1998 - Gregory A. Smith
Last month the Mars Global Surveyor flight team celebrated
as Surveyor completed its 100th orbit around Mars.
- Reference:
Current Flight Status Report (30 Jan 98)
The MGS mission requires the spacecraft to "aerobrake" using the thin
Martian atmosphere to slow the spacecraft and place it into a circular
orbit for mapping.
On 11 October 1997, the Mars Global Surveyor flight team paused the
aerobraking procedures because a damaged solar panel began to bend
backward while passing through a temporarily denser atmosphere than had
been predicted.
After several weeks of analyzing the situation, the flight team decided to
resume aerobraking at a more gentle pace. On 7 November 1997, aerobraking
was resumed, but with the spacecraft's low point to be at an average altitude
of 120km rather than the 110km altitude originally planned. This higher
altitude reduces the air resistance pressure on the spacecraft by 66% but
increases the amount of time required to complete the aerobraking phase.
Under the new mission plan, aerobraking will be suspended in May, 1998 for
six months to allow the spacecraft orbit to drift into a better position
for mapping. During this period, from May 1998 to November 1998, the
spacecraft and flight team will be in a "Science Phasing" period and will
collect as much science as possible to maximize the efficiency of the
mission.
Aerobraking will resume from November 1998 to March 1999 when the
spacecraft will be in its proper mapping orbit. At that point the spacecraft
will circle Mars every two hours and will have a high point of 450km.
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Lunar Prospector
Lunar orbiter
Launch: 6 January 1998
Lunar Arrival: 9 January 1998
Lunar Prospector Home Page
(NASA/Ames Research Center)
Lunar Prospector Mission Control Room
Live WebCam
!
National Space Science Data Center
LANL - History of Space Exploration
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13 February 1998 - Gregory A. Smith
"The Lunar Prospector spacecraft continues to perform very well" -
February 9, 1998 Lunar Prospector Status Report #19.
CONGRATULATIONS LUNAR PROSPECTOR TEAM!
Lunar Prospector successfully launched on January 6, 1998 at 9:28:44 EST.
The Lunar Prospector spacecraft launched from the new Spaceport Florida
commercial launch pad at Cape Canaveral, FL., atop a Lockheed Martin Athena
II launch vehicle.
The spacecraft completed almost three-quarters of a revolution around the
Earth when the Trans Lunar Injection stage fired to put the spacecraft
on a 105 hour coast to the Moon. One minute and 15 seconds after separating
from the third stage of the launch vehicle, all the science instruments were
successfully activated.
The Lunar Prospector will conduct
a low polar orbit investigation of the Moon. Data from the spacecraft will
allow the compositional mapping of the Moon, including possible water ice
deposits trapped in permanently shadowed areas near the lunar poles.
Other instruments will measure the crustal magnetic field, gravity fields
and radon outgassing.
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Deep Space 1
Asteroid, Mars, Comet flyby
Launch: July 1998
Asteroid McAuliffe Flyby:
January 1999
Mars Flyby: April 2000
Comet West-Kohoutek-Ikemura Encounter:
June 2000
Deep Space 1 (JPL)
13 February 1998 - Gregory A. Smith
Deep Space One
is the first deep space mission of NASA's
New Millennium Program.
The New Millennium Program (NMP) is an agressive technology
demonstration
established to validate advanced technologies while returning science
data.
To be launched in July, 1998, Deep Space 1 will validate 12 advanced
technologies and instruments while conducting a flyby of asteroid
McAuliffe, then
Mars
, and finally by comet West-Kohoutek-Ikemura.
"The goal is at least one flight each month" - Kane Casani, manager
of the New Millennium Program.
Reference:
NMP press release - February 10, 1995
(One flight each month will make keeping SPACEUPDATE up-to-date a much more
demanding job!)
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Planet-B
Japanese Mars aeronomy orbiter
Launch: 6 August 1998
Mars Arrival: 11 October 1999
Planet-B
(NSSDC)
13 February 1998 - Gregory A. Smith
Planet-B
is the first Japanese space mission to Mars.
A Mars orbiting aeronomy mission, Planet-B is designed to study the martian upper
atmosphere and its interaction with the solar wind.
Instruments on the spacecraft will
measure the structure, composition and dynamics of the ionosphere, aeronomy effects
of the solar wind, the escape of atmospheric constituents, the structure of the
magnetosphere, and dust in the upper atmosphere and in orbit around Mars. The
mission will also be returning images of Mars' surface and the martian moons
Phobos and Deimos.
Planet-B will initially be put into an elliptical geocentric 7000 km x 400,000 km
parking orbit with its apogee just beyond the orbit of the Moon.
Assuming that launch occurs in the early August launch window as scheduled, the
first lunar swingby will take place in September.
In December it will gain more energy on a second flyby of the Moon, and will then
swing by close to the Earth and slingshot into an escape trajectory
towards Mars. It is scheduled to arrive at Mars on 11 October 1999.
Planet-B will
be inserted into a highly eccentric Mars
orbit 300 km x 47,500 km with an inclination of 138 degrees and a period of just
over 38 hours.
The nominal mission is planned for
one martian year (approximately two Earth years). An extended mission may allow
operation of the mission well beyond the
original two years.
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Mars Surveyor `98 Orbiter
Launch: December 10, 1998
Mars Arrival: September 1999
Mars Surveyor `98 Mission
Mars Surveyor `98 Orbiter Configuration
Mars Surveyor `98 Orbiter
The Mars Surveyor '98 Orbiter will be launched in December of 1998 on a
Delta II rocket. It will be followed about 3 weeks later by the Mars
Surveyor Lander '98, also launched by the same rocket system. Nasa bills
this duo as a "2 for 1" project since one team (at JPL) will supervise both
missions, and much of the hardware is redundant. They also note that with a
mission cap of $184 million both of the '98 Surveyor spacecraft will cost
less than 1997's Mars Pathfinder.
Every 26 months a "transfer opportunity " occurrs because of the alignment
of Earth and Mars. The '98 Surveyor launches take advantage of this window.
The Orbiter spacecraft will have a 10 month journey to the red planet. On
about Sept. 23 1999, it will commence an aerobraking manuver to acheive Mars
orbit insertion (MOI). This eliptical capture orbit will be incrementally
reduced by successive passes through the thin upper atmosphere. After about
2 months the orbit will be circularized using onboard hydrazine thrusters
into a circular polar mapping orbit (altitude ~ 400 km.)
The overall theme of the 2 part Mars Surveyor '98 mission is "volatiles and
climate history". The orbiter's role in this scheme is twofold. Once it
acheives its final orbit it will commence surface mapping, while another
instrument package is analyzing the atmospheric composition and weather. At
the same time it will act as a data link to relay information from its
companion spacecraft (Mars Surveyor '98 Lander) back to Earth. The
atmospheric sounding and imaging phase is scheduled to last for one Mars
year (687 Earth days).
In its role as a data relay the Orbiter should be operational for at least
5 years. This will allow an encore data relay performance for the '01 Mars
mission, arriving in January 2002.
- Jim Warnock
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Mars Surveyor `98 Lander
Launch: January 3, 1999
Mars Landing: December, 1999
Mars Surveyor `98 Mission
Mars Surveyor `98 Lander
While the Mars Surveyor `98 Orbiter surveys the planet from on high, the
Mars Surveyor `98 Lander will conduct its mission from the Martian surface.
The Mars Surveyor `98 Lander must decellerate from 7 km/sec to 2.4 meters/sec
for a safe Martian touchdown. This will be accomplished by aerobraking
with an ablative heatshield, a parachute deployment and a final rocket
propulsion firing for a soft landing. The destination is ~80 degrees S., the first
lander in a polar region. This high latitude region has "layered terrain" which
should have water ice near the surface and might show evidence of past climatic
variations. Certainly new insights will be gained into the seasonal ice
caps (CO2 ice) and polar weather. The lander will have a robotic arm for
trenching, cameras, and atmospheric sensors. Its primary mission is 90 days.
- Jim Warnock
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Deep Space 2
Mars Microprobe Impactors
Launch: January 3, 1999
Mars Landing: December, 1999
Deep Space 2 (JPL)
Deep Space 2 (NSSDC)
NASA New Millennium Program
Piggybacked on the Mars Surveyor `98 Lander spacecraft are 2 "microprobes".
These autonomous impactors are to present many "firsts" for planetary scientists.
The ingenious delivery system saves the money that a dedicated launch would cost
(in the true spirit of hitchhiking!). After 11 months in transit the
microprobes separate from the lander spacecraft for a passive atmospheric
entry. These high tech devices are designed to survive an 80,000 G impact
and be the first probe to gather subsurface data. Once again, investigators
hope to discover clues to Mars' past climate, including the apparent
mystery of the "dissapeared" surface water. Does the water that may have
caused the erosional features we can see today now exist as permafrost? If
so, what implications would that have for possible life forms? Information
on soil temperature, ices, air pressure, and solar measurements will all be
relayed to the Orbiter, which will be overhead 10 times a day to relay the
data back to Earth.
- Jim Warnock
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Stardust
Comet Wild-2 sample return
Launch: February, 1999
Comet Wild-2 Rendezvous:
January, 2004
Earth Return: January, 2006
Stardust Home Page
Stardust (NSSDC)
NASA sample return mission to Comet Wild-2.
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Lunar-A
ISAS (Japan)
Lunar orbiter and penetrator mission
Launch: February 1999
Lunar-A (NSSDC)
LUNAR-A
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MUSES-C
Asteroid 4660 Nereus
lander and sample return
Launch: January 2002
Asteroid Nereus Landing:
September, 2003
Return: January, 2006
MUSES-C (NASA press release)
MUSES-C (NSSDC)
NASA AND JAPAN ASTEROID SAMPLE RETURN MISSION
MUSES-C will be launched on a Japanese
M-5 launch vehicle in January 2002 from Kagoshima Space Center,
Japan and touchdown on the asteroid Nereus in September
2003. A NASA-provided miniature robotic rover will conduct in-
situ measurements on the rocky surface and collect samples.
The asteroid samples will be returned to Earth by MUSES-C via
a parachute-borne recovery capsule in January 2006.
Reference: NASA press release 97-95
- Gregory A. Smith
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CONTOUR
multiple comet mission
Launch: 4-28 July 2002
CONTOUR (NSSDC)
CONTOUR multiple comet mission.
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SELENE
ISAS (Japan)
Lunar orbiter and lander mission
Launch: 2003
Selene (NSSDC)
Selene is an ISAS (Japan) Lunar orbiter and lander mission.
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Rosetta
Comet P/Wirtanen orbiter/rover mission
Launch: January 2003
Mars flyby: July 2005
Earth flyby: November 2005
Asteroid 3840 Mimistrobell flyby:
September 2006
2nd Earth flyby: October 2007
Asteroid 2703 Rodari flyby: May 2008
Comet P/Wirtanen Arrival: August 2012
Rosetta (ESA)
Rosetta (NSSDC)
RoLand rover
Max-Planck-Institut fur Astronomie
Rosetta is a European Space Agency (ESA) mission designed to rendezvous with comet
Wirtanen and perform remote sensing investigations
as well as carrying a probe to land on the comet's surface and perform in
situ measurements. Flybys of two asteroids on the way to the comet, with gravity
assists from Mars and Earth, are also planned.
The mission is named for the Rosetta Stone which was the key to
deciphering Egyptian hieroglyphics. (The stone was named for the
seaside town of Rosetta, Egypt, where it was found by Napoleon's
troops in 1799.)
- Gregory A. Smith
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Deep Space 4/Champollion
Comet Tempel 1 orbiter/lander
Launch: May/June 2003
Champollion/Deep Space 4 Home Page
The Deep Space 4/Champollion mission is designed
to test advanced technologies for landing on
small bodies in the solar system, and for collecting
samples of those bodies and returning them to Earth.
DS4/Champollion will rendezvous with periodic
Comet Tempel 1 in late 2005. After several
months spent studying the cometary nucleus from
orbit, will deploy a 100 kg
spacecraft that will make the first ever landing on
the surface of a comet.
The lander will take close-up images of the
surface and drill one meter into the nucleus to
collect samples of cometary ices and dust. These samples will be examined
by instruments onboard the DS4/Champollion lander and the results
radioed back to Earth. Up to 100 cubic centimeters of
material will be collected and returned to Earth in 2010.
The DS4/Champollion is named after Jean Francois Champollion, a
French Egyptologist who, collaborating with Thomas Young, deciphered
the ancient Egyptian hieroglyphic and demotic text on the stone by
comparing it with the known Greek text on the same stone.
- Gregory A. Smith
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