ESA Document - Emits - ESA
ESA Document - Emits - ESA ESA Document - Emits - ESA
s Figure 4-39: Power required to maintain temperature HMM Assessment Study Report: CDF-20(A) February 2004 page 288 of 422 The insulating system is assumed to provide an equivalent thermal conductivity of 0.13W/m 2 /K (15 cm of foam). Therefore, maintaining over one sol an internal wall above dew point (14C for 75% humidity, mean sink –60C + 20C margin accounting to heat losses through inertia) would require a power density of 11.3W/m 2 . Two systems are proposed: • a network of heaters homogeneously distributed on the internal shell corresponding to a installed power of 728W (assuming the SHM as a cylinder 3.6 x 5.7 m length). Two equivalent circuits (main and redundant) are foreseen, each piloted by a control unit. For safety, each circuit will be equipped with over temperature thermostats to protect against a failed-on heater switch. • a network of coils / heat pipes mounted on the internal shell to transfer / homogenize the rejected heat from main loop (about 2.7 kW) A strategy for heater power saving can be implemented with a pre-heating before the night (using the higher activity dissipation during the day through the fluid heat storage capability). Local PCM (where worst heat leaks are located) can also efficiently complete the system. An optimised heat management could request little electrical power to maintain the requirements. For safety reasons, however, a certain provision of installed power shall be designed (about 728W). No particular trade-off has been done on the landing location assuming no specific landing (polar site or winter period with high latitude). 4.3.4.3.5 Overview
s Insulation structure (external) Foam + betacloth Window shutter (int.) thermal insulation during night Insulation legs (ext.): aluminium foil where no mechanism Insulation oxygen tanks (int.) + cryocooling Insulation of the hatches 4.3.4.3.6 Fuel cells Figure 4-40: Thermal system configuration Heating system (internal) Primary loop + coil system (int.) Secondary loop system (int.) pump, heat exchanger HMM Assessment Study Report: CDF-20(A) February 2004 page 289 of 422 Body mounted radiator (ext.) lateral cylinder of 10 m 2 (2 m high), white painted Insulation of the bottom + protection versus plumes Because of its high energy density, hydrogen is normally retained as the fuel and oxygen as its reactant. Related technologies regarding the electrolytes have been addressed in the power section. Whichever choice, thermal management of the fuel cells is essential: • to guarantee the operating temperature of the chemical reaction • to preheat the cryogenics reactants before entering the stacks • to cool down each stack, because of the highly exothermic chemical reaction (141.9 MJ/kg) The cooling capability of the stacks is provided by a coil system connected to the coldest sink through a dedicated secondary loop heat exchanger. The fluid used for this loop is a fluorinated hydrocarbon coolant. A temperature actuated flow control valve maintains and regulates the coolant exit temperature. As preliminary inputs for heating power, the PEM cells used in the STS (7 kW per unit) are assumed with 2.4 kW for start up and 1.1 kW in nominal mode. Note that, the water by-product used for life support can be used also as a coolant in the thermal management system. An integrated system (thermal / power / life support) possibly based on regenerative cells seems promising for mass saving (transfer vehicle for instance). 4.3.4.3.7 Cryogenic storage for fuel cells tanks Fuel cells are used for the MEV require the storage of liquid hydrogen and oxygen, and an appropriate thermal design to maintain the related boil-off (BO) to an acceptable level. The objective is to have after 24 months, 119 kg of hydrogen and 955 kg of oxygen (input from power subsystem). The tanks are identical in shape and their geometry is a sphere. They are located in an unpressurised section of the MEV to minimise parasitic heat transfer from surrounding elements (gas conduction). Passive insulation is used to isolate the tanks from their radiative environment. The MLI is a stack of n layers of Double Aluminized Mylar (DAM) with an external goldenized layer.
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s<br />
Figure 4-39: Power required to maintain temperature<br />
HMM<br />
Assessment Study<br />
Report: CDF-20(A)<br />
February 2004<br />
page 288 of 422<br />
The insulating system is assumed to provide an equivalent thermal conductivity of 0.13W/m 2 /K<br />
(15 cm of foam). Therefore, maintaining over one sol an internal wall above dew point (14C for<br />
75% humidity, mean sink –60C + 20C margin accounting to heat losses through inertia) would<br />
require a power density of 11.3W/m 2 .<br />
Two systems are proposed:<br />
• a network of heaters homogeneously distributed on the internal shell corresponding to a<br />
installed power of 728W (assuming the SHM as a cylinder 3.6 x 5.7 m length). Two<br />
equivalent circuits (main and redundant) are foreseen, each piloted by a control unit. For<br />
safety, each circuit will be equipped with over temperature thermostats to protect against<br />
a failed-on heater switch.<br />
• a network of coils / heat pipes mounted on the internal shell to transfer / homogenize the<br />
rejected heat from main loop (about 2.7 kW)<br />
A strategy for heater power saving can be implemented with a pre-heating before the night<br />
(using the higher activity dissipation during the day through the fluid heat storage capability).<br />
Local PCM (where worst heat leaks are located) can also efficiently complete the system. An<br />
optimised heat management could request little electrical power to maintain the requirements.<br />
For safety reasons, however, a certain provision of installed power shall be designed (about<br />
728W). No particular trade-off has been done on the landing location assuming no specific<br />
landing (polar site or winter period with high latitude).<br />
4.3.4.3.5 Overview