Editing Phobos 2 (section)

==Spacecraft design==
===Instruments===

The ''Phobos 2'' [[Thermal infrared spectroscopy|infrared spectrometer]] (ISM) obtained 45000 spectra in the near infrared (from {{val|0.75|to|3.2|u=um}}) in the equatorial areas of Mars, with a spatial resolution ranging from {{val|7|to|25|u=km}}, and 400 spectra of Phobos at 700 m resolution. These observations made it possible to generate the first mineralogical maps of the planet and its satellite, and to study the atmosphere of Mars. ISM was developed at [[Institut aéronautique et spatial|IAS]] and [[DESPA]] ([[Paris Observatory]]) with support from [[CNES]].

List of instruments:
* "VSK" TV imaging system
* PROP-F "hopping" lander.
**ARS-FP automatic X-ray fluorescence spectrometer
**ferroprobe [[magnetometer]]
**Kappameter magnetic permeability / susceptibility sensor
**gravimeter
**temperature sensors
**BISIN conductometer / tiltmeter
**mechanical sensors (penetrometer, UIU accelerometer, sensors on hopping mechanism)
*"DAS" (long-lived autonomous station) lander
**TV camera
**ALPHA-X Alpha-Proton-X-Ray Spectrometer
**LIBRATION [[Sun sensor]] (also known as STENOPEE)
**Seismometer
**RAZREZ anchor penetrometer
**Celestial mechanics experiment
* "ISM" thermal infrared spectrometer/radiometer - {{val|1|2|u=km}} resolution
* near-infrared imaging spectrometer
* thermal imaging camera; magnetometers
* gamma-ray spectrometers
* X-ray telescope
* radiation detectors
* radar and laser altimeters
* Lima-D laser experiment - designed to vaporize material from the Phobos surface for chemical analysis by a mass spectrometer
* Automatic Space Plasma Experiment with Rotating Analyzer (ASPERA), an electron spectrometer and ion mass analyzer from the [[Swedish Institute of Space Physics]].