Information AboutVoyager Program |
| CATEGORIES ABOUT VOYAGER PROGRAM | |
| jupiter | |
| saturn | |
| uranus | |
| neptune | |
| voyager program | |
| nasa programsjupiter | |
| saturn | |
| uranus | |
| neptune | |
| voyager program | |
| nasa programs | |
| nasa probes | |
|
The Voyager program consists of a pair of unmanned scientific Probe s, Voyager 1 and Voyager 2 , launched in 1977 . They were sent to study Jupiter and Saturn , using an advantageous planetary alignment of the late 1970s . However, the mission planners always had in the back of their minds a continued mission into the Outer Solar System ; and Voyager 2 eventually went on to examine Uranus and Neptune . They were originally conceived as part of the Mariner Program , being Mariner 11 and Mariner 12 respectively. The original program name was '''Mariner Jupiter-Saturn'''. It was later given the more appealing and romantic name "Voyager". Voyager was actually a scaled back version of the Grand Tour program of the late 1960s and early 1970s to send a pair of probes to fly by all the outer planets (scaled back because of budget cuts). In the end, it fulfilled all the Grand Tour flyby objectives save Pluto despite not being officially designed for such a long duration mission. Both missions gathered large amounts of data about the Gas Giant s of the Solar System . In addition, the spacecraft trajectories have been used to place limits on the existence of a hypothetical post- Pluto nian Planet X . In the 1990s Voyager 1 overtook the slower travelling Pioneer 10 to become the most distant human made artifact in space - a record it will keep for at least several more decades (the faster New Horizons probe will catch up in about 200 years). Voyager 1 and Pioneer 10 are also the most widely-separated man made objects in the Universe because they are travelling in roughly opposite directions from the sun. in late 2004]] Periodic contact has been maintained with both probes to monitor conditions in the outer expanses of the solar system. The crafts' Radioactive power sources are still producing electrical energy, fuelling hopes of locating our solar system's Heliopause . In late 2003 , Voyager 1 began sending data that seemed to indicate it had crossed the Termination Shock , but interpretations of this data were in dispute. It is now believed that the termination shock was crossed in December, 2004, with the heliopause an unknown distance ahead. Due to budget shifts prompted by , before they observe the Heliopause , disappointing many scientists. However the program continues to be funded into 2006. These probes were built at JPL funded by NASA . Attached to each of them is a copy of the Voyager Golden Record . VOYAGER SPACECRAFT DESIGN AND INSTRUMENTATION The identical Voyager spacecraft are three- Axis stabilized systems that use Celestial or Gyro referenced Attitude Control to maintain pointing of the High-gain Antenna s toward Earth . The prime mission science payload consisted of 10 instruments (11 investigations including Radio Science ). Only five investigator teams are still supported, though data are collected for two additional instruments. The Flight Data Subsystem (FDS) and a single eight-track ''' Digital Tape Recorder ''' (DTR) provide the data handling functions. The FDS configures each instrument and controls instrument operations. It also collects engineering and science data and formats the data for Transmission . The DTR is used to record high-rate ''' Plasma Wave Subsystem''' (PWS) data. Data are played back every six months. The Imaging Science Subsystem, made up of a wide angle and a narrow angle camera, is a modified version of the slow scan Vidicon camera designs that were used in the earlier Mariner flights. The Imaging Science Subsystem '''Narrow Angle Camera''' consists of two television-type cameras, each with 8 filters in a commandable Filter Wheel mounted in front of the vidicons. One has a low resolution 200 mm wide-angle lens with an aperture of f/3, while the other uses a higher resolution 1500 mm narrow-angle f/8.5 lens. Unlike the other onboard instruments, operation of the cameras is not autonomous, but is controlled by an imaging parameter table residing in one of the spacecraft computers, the Flight Data Subsystem (FDS). The computer command subsystem (CCS) provides sequencing and control functions. The CCS contains fixed routines such as command decoding and fault detection and corrective routines, antenna pointing information, and spacecraft sequencing information. The Attitude and Articulation Control Subsystem (AACS) controls the spacecraft orientation, maintains the pointing of the High-gain Antenna towards Earth, controls attitude maneuvers, and positions the scan platform. Uplink communications is via S Band (16- Bit/s command rate) while an X Band transmitter provides downlink telemetry at 160 bit/s normally and 1.4 kbit/s for playback of high-rate plasma wave data. All data are transmitted from and received at the spacecraft via the 3.7-meter high-gain antenna (HGA). Electrical Power is supplied by three Radioisotope Thermoelectric Generator s (RTGs). The current power levels are about 315 W for each spacecraft. As the electrical power decreases, power loads on the spacecraft must be deactivated in order to avoid exceeding its remaining power supply. As loads are turned off, some spacecraft capabilities are eliminated. To date, the entire Voyager 2 and Voyager 1 scan platform, including all of the platform instruments, has been powered down. The '''ultraviolet spectrometer''' (UVS) {Link without Title} on Voyager 1 was on until 2003 , when it too was deactivated. Gyro operations will end in 2010 for Voyager 2 and 2011 for Voyager 1. Gyro operations are used to rotate the probe 360 degrees 6 times a year. This is used to measure the Magnetic Field of the spacecraft, which is then subtracted from the Magnetometer science data. The two Voyager spacecraft continue to operate, with some loss in subsystem redundancy, but retain the capability of returning science data from a full complement of VIM science instruments. Both spacecraft also have adequate electrical power and attitude control propellant to continue operating until around 2020 when the available electrical power will no longer support science instrument operation. At this time science data return and spacecraft operations will cease. The radioisotope thermoelectric generators are powered by Plutonium , and provided approximately 470 W of 30- Volt DC when the spacecraft was launched. Plutonium-238 decays with a Radioactive half-life of approximately 85 years, so RTGs using it lose a factor of of their power output per year, approximately 0.81%. 23 years after launch, such an RTG would produce only 470 W × 0.991923 ~= 390 W — or roughly 83% — of the initial power. However, the bi-metallic Thermocouple s used to convert Thermal Energy into Electrical Energy degrade as well; at the beginning of 2001 , the power generated by Voyager 1 and Voyager 2 had dropped to 315 W and to 319 W respectively, about 80% of the power output at launch. Both of these power levels represent better performance than the pre-launch predictions, which included a conservative degradation model for the thermocouples. GOLDEN RECORD ''Voyager 1'' carries with it a golden record ( ''Voyager'' Golden Record ) that contains pictures and sounds of Earth, along with symbolic directions for playing the record and data detailing the location of Earth. The record is intended as a combination time capsule and interstellar message to any civilization, alien or far-future human, that recovers ''Voyager 1''. The contents of this record were selected by a committee chaired by Carl Sagan . VOYAGER IN FICTION AND POPULAR CULTURE The section Voyager 2 In Fiction And Popular Culture in the Voyager 2 article contains specific references to Voyager 2 in pop culture.
SEE ALSO
There is a facilities to improve communication with craft in the Voyager program. EXTERNAL LINKS
|
|
|