.mw-parser-output .hidden-begin{box-sizing:border-box;width:100%;padding:5px;border:none;font-size:95%}.mw-parser-output .hidden-title{font-weight:bold;line-height:1.6;text-align:left}.mw-parser-output .hidden-content{text-align:left}You can help expand this article with text translated from the corresponding article in Russian. (November 2020) Click [show] for important translation instructions.
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| Transport and Energy Module (TEM) | |
|---|---|
 | |
| Generation | Generation IV |
| Reactor concept | Gas-cooled reactor (GCR) |
| Designed by | Keldysh Research Center Rosatom Roscosmos NIKIET institute |
| Manufactured by | Keldysh Research Center NIKIET institute |
| Status | Under development |
| Main parameters of the reactor core | |
| Fuel (fissile material) | Information missing |
| Fuel state | Solid |
| Neutron energy spectrum | Thermal |
| Primary coolant | helium 78% - xenon 22% [1] |
| Reactor usage | |
| Primary use | Generation of electricity for propulsion |
| Power (thermal) | 3.8 MW |
| Power (electric) | 1 MWe (BWR-1) |
TEM (Russian: Транспортно-энергетический модуль, "transport and energy module\unit", NPPS in English) is an under development nuclear propulsion spacecraft with the intention to facilitate the transportation of large cargoes in deep space.[2] It will be constructed by the Russian Keldysh Research Center,[3] NIKIET (Research and Design Institute of Power Engineering) institute,[4] and Rosatom.
