LWRHULightweight Radioisotope Heater Unit
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References in periodicals archive ?
The NASA jet propulsion laboratory has developed a light-weight RHU (LWRHU) for space applications [14].
This was estimated from the thermal analysis results shown in Table 6 under the assumption that an LWRHU [14] with the output power of 1 W and mass of 40 g per unit was used for the lander.
Tate, "Light weight radioisotope heater unit (LWRHU): a technical description of the reference design," Los Alamos National Laboratory, LA-9078-MS, 1982.