- International Cometary Explorer
Name = ICE (ISEE-3)
Caption = ICE (ISEE-3)
Earth/ MoonL1 libration point orbiter, Giacobini-Zinner & Comet Halleyflyby
August 12, 1978
Launch_Vehicle = Delta
Mission_Duration = May
Mass = 390 kg
NSSDC_ID = 1978-079A
Webpage = [http://nssdc.gsfc.nasa.gov/space/isee.html ISEE project page]
Eccentricity = .05
Inclination = .1°
Orbital_Period = 355 d
Apoapsis = 1.03 AU
Periapsis = .93 AU
The International Cometary Explorer (ICE)
spacecraftwas originally known as International Sun/Earth Explorer 3 (ISEE-3) satellite, launched August 12, 1978. It was part of the ISEE ( International Sun-Earth Explorer) international cooperative program between NASAand ESAto study the interaction between the Earth's magnetic fieldand the solar wind. The program used three spacecraft, a mother/daughter pair ( ISEE 1and ISEE 2) and a heliocentricspacecraft (ISEE 3, later renamed ICE).
ICE was the first spacecraft to be placed in a heliocentric
halo orbit. It was later sent to visit Comet Giacobini-Zinner and Comet Halley, and was the first spacecraft to visit more than one comet.
Original mission: International Sun/Earth Explorer 3 (ISEE-3)
ISEE-3 originally operated in a "halo" orbit about the L1 Sun-Earth
Lagrangian point. It was the first artificial object placed at a so-called "libration point", proving that such a suspension between gravitational fields was possible.
The purposes of the mission were:
* to investigate solar-terrestrial relationships at the outermost boundaries of the Earth's magnetosphere;
* to examine in detail the structure of the solar wind near the Earth and the shock wave that forms the interface between the solar wind and Earth's magnetosphere;
* to investigate motions of and mechanisms operating in the plasma sheets; and,
* to continue the investigation of cosmic rays and solar flare emissions in the interplanetary region near 1 AU.
The Explorer-class heliocentric spacecraft, International Sun-Earth Explorer 3, was part of the mother/daughter/heliocentric mission (ISEE 1, 2, and 3).The three spacecraft carried a number of complementary instruments for making measurements of plasmas, energetic particles, waves, and fields.
This heliocentric spacecraft had a spin axis normal to the ecliptic plane and a spin rate of about 20 rpm. It was initially placed into an elliptical halo orbit about the L1 libration point 235 Earth radii (approximately 1.5 million km, or 932,000 miles) on the sunward side of the Earth, where it continuously monitored changes in the near-Earth interplanetary medium.
econd mission: International Cometary Explorer
June 10, 1982, after completing its original mission, ISEE-3 was repurposed. It was renamed the International Cometary Explorer (ICE). The primary scientific objective of ICE was to study the interaction between the solar wind and a cometary atmosphere. After a successful thruster burn to knock it loose from its halo orbit on September 1of that year, it used the instability of the Earth/Moon and Earth/Sun Lagrange points, making a series of lunar orbits over the next 15 months. Its last and closest pass over the Moon, on December 22, 1983, was a mere 119.4 km above the moon's surface. By the beginning of 1984, ICE was in heliocentric orbit.
After ejection out of the Earth-Moon system, ICE entered a heliocentric orbit ahead of the Earth on a trajectory intercepting that of Comet Giacobini-Zinner. On
11 September, 1985, the craft passed through the plasma tail of Comet Giacobini-Zinner. Due to the nature of its original mission, ICE carried no cameras. It instead carried instruments for measurements of energetic particles, waves, plasmas, and fields.
ICE transited between the Sun and Comet Halley in late March
1986, when other spacecraft (Giotto, Vega 1 and 2, Suisei and Sakigake) were also in the vicinity of Comet Halleyon their early March comet rendezvous missions (see Halley Armada). ICE became the first spacecraft to directly investigate two comets.
An update to the ICE mission was approved by NASA in 1991. It defines a Heliospheric mission for ICE consisting of investigations of
coronal mass ejectionsin coordination with ground-based observations, continued cosmic raystudies, and the Ulysses probe. By May 1995ICE was being operated with only a low duty cycle, with some support being provided by the Ulysses project for data analysis. Two years later, termination of operations of ICE/ISEE3 was authorized May 5, 1997.
End of mission
Termination of operations of ICE/ISEE3 was authorized
May 5, 1997.
The ISEE-3/ICE downlink bit rate was nominally 2048 bit/s during the early part of the mission, and 1024 bit/s during the Giacobini-Zinner comet encounter. The bit rate then successively dropped to 512 bit/s (on
1985-12-09), 256 bit/s (on 1987-01-05), 128 bit/s (on 1989-01-24) and finally to 64 bit/s (on 1991-12-27).
As of January
1990, ICE was in a 355 day heliocentricorbit with an aphelionof 1.03 AU, a perihelionof 0.93 AU and an inclination of 0.1 degree. It may be possible to capture the spacecraft in 2014, when it again makes a close approach to Earth. If the craft is recovered, it has already been donated by NASA to the Smithsonian Institution.
On 18 September
2008, contact was reestablished with the spacecraft by the Deep Space Network. NASA scientists are in pre-planning proposal mode for a mission which considers reusing the probe to observe additional comets in 2017or 2018. [ [http://www.planetary.org/blog/article/00001673/ The Planetary Science Weblog - "It's Alive!"] ]
* [http://nssdc.gsfc.nasa.gov/space/isee.html ISEE project page]
* [http://agile.gsfc.nasa.gov/docs/heasarc/missions/isee3.html Nasa/HEASARC Mission Overview]
* [http://solarsystem.nasa.gov/missions/profile.cfm?MCode=ISEEICE ISEE-3/ICE Mission Profile] by [http://solarsystem.nasa.gov NASA's Solar System Exploration]
* [http://www.daviddarling.info/encyclopedia/I/International_Cometary_Explorer.html Encyclopedia of Astrobiology Astronomy and Spaceflight]
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