Space vehicle apparatus including a cellular sandwich with phase change material
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorEdward S. Hickey
Life of this patent
Estimating the term…
Abstract
Apparatus for holding a space vehicle at a constant temperature including llular sandwich on the outer surface of the space vehicle, the cellular sandwich having two outer layers and translucent cells between the two outer layers, the translucent cells containing phase change material, the outer layer that is more distant from the space vehicle able to transmit sunlight to the translucent cells and able to transmit radiation away from the translucent cells, the phase change material absorbing sunlight and radiating energy to maintain the space vehicle at a constant temperature in sunlight and darkness.
Claims3
Apparatus for holding a space vehicle at a constant temperature during space flight, comprising:
- (a) the space vehicle;
- (b) a cellular sandwich having outer layers, the cellular sandwich on an outer surface of the space vehicle, the cellular sandwich having translucent cells interior to the outer layers, an outer layer that is more distant from the space vehicle being able to transmit sunlight to the translucent cells and to transmit radiation from the translucent cells;
- and
- (c) a selected amount of the phase change material within the translucent cells of the cellular sandwich, the phase change material absorbing sunlight and radiating energy for holding the space vehicle at a constant temperature during a space flight.
Apparatus for maintaining a space vehicle at a first temperature state for a first period of time while the space vehicle is in sunlight and for maintaining the space vehicle at a second temperature state for a second period of time while the space vehicle is in dark space, during space flight, comprising:
- (a) a cellular sandwich having outer layers, the cellular sandwich on an outer surface of the space vehicle, the cellular sandwich having translucent cells interior to the outer layers, an outer layer that is more distant from the space vehicle being able to transmit sunlight to the translucent cells and to transmit radiation from the translucent cells;
- (b) a selected amount of the phase change material being a first phase change material within each of selected translucent cells of the cellular sandwich, the selected amount of the first phase change material absorbing sunlight and radiating energy for maintaining the space vehicle at a first temperature state for a first period of time while the space vehicle is in sunlight;
- and
- (c) a selected amount of the phase change material being a second phase change material within each of the other selected translucent cells of the cellular sandwich, the selected amount of the second phase change material absorbing sunlight and radiating energy for maintaining the space vehicle at a second temperature state for a second period of time while the space vehicle is in dark space.
Apparatus for holding a space vehicle in a first constant temperature state in sunlight and in a second constant temperature state in dark space, during space flight, comprising:
- (a) the space vehicle;
- (b) a conic cellular sandwich having conic outer layers, the conic cellular sandwich on a conic outer surface of the space vehicle, the conic cellular sandwich having translucent cells, an outer layer that is more distant from the space vehicle being able to transmit sunlight to the translucent cells and to transmit radiation from the translucent cells;
- (c) a first selected amount of the phase change material being a first phase change material within some cells of the conic cellular sandwich, the first phase change material absorbing sunlight and radiating energy for holding the vehicle at a first temperature state in sunlight;
- and
- (d) a second selected amount of the phase change material being a second phase change material within other cells of the conic cellular sandwich, the second phase change material absorbing sunlight and radiating energy for holding the vehicle at a second temperature state in dark space.
Dependencies are inferred from the claim text.