Water may be used as radiation shielding for Solar Particle Events (SPE) to protect crewmembers in the Lunar Electric Rover (LER). Because the water is already present for radiation protection, it could also provide a mass efficient solution to the vehicle's thermal control system. This water can be frozen by heat rejection from a radiator and used as a Phase Change Material (PC1V1) for thermal storage. Use of this water as a PCM can eliminate the need for a pumped fluid loop thermal control system as well as reduce the required size of the radiator. This paper describes the testing and analysis performed for the Rover Engineering Development Unit (REDU), a scaled-down version of a water PCM heat sink for the LER. The REDU was tested in a t...
Future lunar landers and rovers will require variable thermal links that allow for heat rejection du...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
Phase change materials (PCM) may be useful for thermal control systems that involve cyclical heat lo...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
Supplemental heat rejection devices are required in many spacecraft as the radiators are not sized t...
In low Lunar orbit (LLO) the thermal environment is cyclic - extremely cold in the eclipse and as wa...
During an ExtraVehicular Activity (EVA), both the heat generated by the astronaut's metabolism and t...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
Abstract. Nuclear power systems for long-term Lunar and Martian missions present many challenges to ...
Thermal wadis, engineered sources of heat, can be used to extend the life of lunar rovers by keeping...
A flight experiment is being constructed to utilize the persistent microgravity environment of the I...
NASA's Orion Multipurpose Crew Vehicle's Exploration Mission 2 is expected to loiter in Lunar orbit ...
Radiator panels utilizing titanium-water heat pipes are being considered for lunar applications. A t...
During my internship in the Thermal Design Branch (ES3), I contributed to two main projects: i) nove...
Future lunar landers and rovers will require variable thermal links that allow for heat rejection du...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
Phase change materials (PCM) may be useful for thermal control systems that involve cyclical heat lo...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
Supplemental heat rejection devices are required in many spacecraft as the radiators are not sized t...
In low Lunar orbit (LLO) the thermal environment is cyclic - extremely cold in the eclipse and as wa...
During an ExtraVehicular Activity (EVA), both the heat generated by the astronaut's metabolism and t...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
Abstract. Nuclear power systems for long-term Lunar and Martian missions present many challenges to ...
Thermal wadis, engineered sources of heat, can be used to extend the life of lunar rovers by keeping...
A flight experiment is being constructed to utilize the persistent microgravity environment of the I...
NASA's Orion Multipurpose Crew Vehicle's Exploration Mission 2 is expected to loiter in Lunar orbit ...
Radiator panels utilizing titanium-water heat pipes are being considered for lunar applications. A t...
During my internship in the Thermal Design Branch (ES3), I contributed to two main projects: i) nove...
Future lunar landers and rovers will require variable thermal links that allow for heat rejection du...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...
In a cyclical heat load environment such as low Lunar orbit, a spacecraft's radiators are not sized ...