Integrated Science Instrument Module

Integrated Science Instrument Module (ISIM) is a component of the James Webb Space Telescope, a large international infrared space telescope planned for launch in 2018. ISIM is the heart of the JWST, and holds the main science payload which includes four science instruments and the fine guidance sensor. ISIM is the spacecraft chassis and instruments that take the light from the main mirror and convert that into the science data that is then sent back to Earth. The other two major sections of the JWST are the Optical Telescope Element (OTE) (mirror and their structure) and the Spacecraft Element (SE), which includes the Spacecraft Bus and Sunshield. ISIM has a mass of 1.4 metric tons (tonnes) (1.54 US tons). The infrared camera instrument integrated with ISIM passed its thermal tests in early 2016. ISIM underwent intense thermal cold testing in late 2015 to early 2016. NIRcam is extremely important to JWST, because it's not only a sensitive infrared camera, but it is also used to adjust the alignment of the main mirror segments. The tests were very positive because NIRcam showed was very stable through vibration and thermal testing. NIRcam was installed into ISIM in March 2014, and then underwent integration and testing after that, as the telescope is readied for its 2018 launch. ISIM is about 23% of the overall mass of JWST, which equates to an ISIM mass of 1400 kg (3086 lb).

ISIM contains these instruments:

ISIM also includes the MIRI crycooler, which extends down into the Spacecraft Bus (on the hot side of the spacecraft). Relevant systems and subsystems the ISIM:

Three regions to ISIM were defined by NASA to aid in its production. The three regions include the cryogenic instrument module (1), the electronics compartment (2), and finally the Command and Data Handling subsystem and MIRI crycooler(3), which is inside the spacecraft bus physically. MIRI needs to be colder than the other instruments so it has an additional cooler. MIRI is the mid-infrared instrument. The Command and Data Handling subsystem uses the in-spaceship communication standard called SpaceWire. SpireWire was jointly developed by the ESA and NASA, and includes a low-power microchip that can send data at 200 mbits per second.

Regions:

The ISIM Electronics Compartment (IEC) is a section of ISIM that houses computing and electrical resources for the instruments. The main electronics for each of the instruments is housed in this thermally wrapped box. In 2014 the electronics for NIRspec were installed in the IEC. The IEC is mounted to the cryogenic structure of the main telescope, and the enclosure must maintain a much warmer temperature for the electronics inside, but not allow that heat to negatively affect the main telescope. The box can dissipate about 200 watts of electrical power. One of the considerations is to direct the majority of the heat (radiatively) in a roughly 20 degree angle in between the back of the main mirror structure and instruments and the sunshield. Not too close to the back of the telescope or too close to the sunshield, but by using baffles and insulation, direct the heat out into space. The IEC box sits just below most of the instruments and behind it, but above the spacecraft bus.

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