Международный кометарный исследователь (ICE): История космического аппарата

NASA satellite of the Explorer program

The International Cometary Explorer (ICE) spacecraft (designed and launched as the International Sun Earth Explorer 3 (ISEE 3) satellite), was launched 12 August 1978, into a heliocentric orbit. It was one of three spacecraft, along with the mother/daughter pair of ISEE 1 and ISEE 2, built for the International Sun Earth Explorer (ISEE) program, a joint effort by NASA and ESRO/ESA to study the interaction between the Earth's magnetic field and the solar wind. ISEE 3 was the first spacecraft to be placed in a halo orbit at the Earth Sun Lagrange point. Renamed ICE, it became the first spacecraft to visit a comet, passing through the plasma tail of comet Giacobini Zinner within about of the nucleus on 11 September 1985. NASA suspended routine contact with ISEE 3 in 1997, and made brief status checks in 1999 and 2008. On 29 May 2014, two way communication with the spacecraft was reestablished by the ISEE 3 Reboot Project, an unofficial group, with support from the Skycorp company and SpaceRef Interactive. On 2 July 2014, they fired the thrusters for the first time since 1987. However, later firings of the thrusters failed, apparently due to a lack of nitrogen pressurant in the fuel tanks. The project team initiated an alternative plan to use the spacecraft to "collect scientific data and send it back to Earth", but on 16 September 2014, contact with the probe was lost.

ISEE 3 carries no cameras; instead, its instruments measure energetic particles, waves, plasmas, and fields. ISEE 3 originally operated in a halo orbit about the Sun Earth Lagrange point, 235 Earth radii above the surface (about It was the first artificial object placed at a so called "libration point", entering orbit there on 20 November 1978, Fifteen propulsive maneuvers and five lunar gravity assists resulted in the spacecraft being ejected from the Earth Moon system and into a heliocentric orbit. Its last and closest pass over the Moon, on December 22, 1983, was only above the lunar surface; following this pass, the spacecraft was re designated as the International Cometary Explorer (ICE).

Its new orbit put it ahead of the Earth on a trajectory to intercept comet Giacobini Zinner. On 11 September 1985, the craft passed through the comet's plasma tail.

ICE transited between the Sun and Comet Halley in late March 1986, when other spacecraft were near the comet on their early March comet rendezvous missions. (This "Halley Armada" included Giotto, Vega 1 and 2, Suisei and Sakigake.) ICE flew through the tail; its minimum distance to the comet nucleus was For comparison, Earth's minimum distance to Comet Halley in 1910 was .

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 ejections in coordination with ground based observations, continued cosmic ray studies, and the Ulysses probe. By May 1995, ICE was being operated under a low duty cycle, with some data analysis support from the Ulysses project.

On 5 May 1997, NASA ended the ICE mission, leaving only a carrier signal operating. The ISEE 3/ICE downlink bit rate was nominally 2048 bits per second during the early part of the mission, and 1024 bit/s during the 21P/Giacobini–Zinner comet encounter. The bit rate then successively dropped to 512 bit/s (on 9 December 1985), 256 bit/s (on 5 January 1987), 128 bit/s (on 24 January 1989) and finally to 64 bit/s (on 27 December 1991). Though still in space, NASA donated the craft to the Smithsonian Museum. By January 1990, ICE was in a 355 day heliocentric orbit with an aphelion of 1.03 AU, a perihelion of 0.93 AU and an inclination of 0.1°.

In 1999, NASA made brief contact with ICE to verify its carrier signal. On 18 September 2008, NASA, with the help of KinetX, located ICE using the NASA Deep Space Network after discovering that it had not been powered off after the 1999 contact. A status check revealed that 12 of its 13 experiments were still functioning, and it still had enough propellant for of Δv. It was determined to be possible to reactivate the spacecraft in 2014, when it again made a close approach to Earth, and scientists discussed reusing the probe to observe more comets in 2017 or 2018.

Sometime after NASA's interest in the ICE waned, others realized that the spacecraft might be steered to pass close to another comet. A team of engineers, programmers, and scientists began to study the feasibility and challenges involved. On 15 May 2014, the project reached its crowdfunding goal of US$125,000 on RocketHub, which was expected to cover the costs of writing the software to communicate with the probe, searching through the NASA archives for the information needed to control the spacecraft, and buying time on the dish antennas. The project then set a "stretch goal" of US$150,000, which it also met with a final total of US$159,502 raised. The project members were working on deadline: if they got the spacecraft to change its orbit by late May or early June 2014, or in early July by using more fuel, it could use the Moon's gravity to get back into a useful halo orbit.

Earlier in 2014, officials with the Goddard Space Flight Center said the NASA Deep Space Network equipment necessary to transmit signals to the spacecraft had been decommissioned in 1999, and was too expensive to replace. However, project members were able to find documentation for the original equipment and were able to simulate the complex modulator/demodulator electronics using modern software defined radio (SDR) techniques and open source programs from the GNU Radio project. They obtained the needed hardware, an off the shelf SDR transceiver, and power amplifier, and installed it on the Arecibo dish antenna on 19 May 2014. Once they gained control of the spacecraft, the capture team planned to shift the primary ground station to the dish located at Morehead State University Space Science Center of Kentucky.

On 29 May 2014, the reboot team successfully commanded the probe to switch into Engineering Mode to begin to broadcast telemetry. On 26 June 2014, project members using the Goldstone Deep Space Communications Complex DSS 24 antenna achieved synchronous communication and obtained the four ranging points needed to refine the spacecraft's orbital parameters. The project team received approval from NASA to continue operations through at least 16 July 2014, and made plans to attempt the orbital maneuver in early July. On 2 July 2014, the reboot project fired the thrusters for the first time since 1987. They spun up the spacecraft to its nominal roll rate, in preparation for the upcoming trajectory correction maneuver in mid July. On 8 July 2014, a longer sequence of thruster firings failed, apparently due to loss of the nitrogen gas needed to pressurize the fuel tanks. On 30 July 2014, the team announced that it still planned to acquire data from as much of ISEE 3's 300 day orbit as possible. With five of the 13 instruments on the spacecraft still working, the science possibilities included listening for gamma ray bursts, where observations from additional locations in the Solar System can be valuable. The team was also recruiting additional receiving sites around the globe to improve diurnal coverage, in order to upload additional commands while the spacecraft is close to Earth and later to receive data. On 10 August 2014 at 18:16 UTC, the spacecraft passed about from the surface of the Moon. It will continue in its heliocentric orbit, and will return to the vicinity of Earth in 2031.

On 25 September 2014, the Reboot team announced that contact with the probe was lost on 16 September 2014. It is unknown whether contact can be reestablished because the probe's exact orbit is uncertain. The spacecraft's post lunar flyby orbit takes it further from the Sun, causing electrical power available from its solar arrays to drop, and its battery failed in 1981. Reduced power could have caused the craft to enter a safe mode, from which it may be impossible to awaken without the precise orbital location information needed to point transmissions at the craft. It has a dry mass of and can generate nominal power of 173 watts.

ICE carries 13 scientific instruments to measure plasmas, energetic particles, waves, and fields. as of 2014, five were known to be functional. It does not carry a camera or imaging system. Its detectors measure high energy particles such as X and gamma rays, solar wind, plasma and cosmic particles. A data handling system gathers the scientific and engineering data from all systems in the spacecraft and formats them into a serial stream for transmission. The transmitter output power is five watts.