Gemini Fuel Cell
The first time a fuel cell was used on a U.S. manned space flight was in the
Gemini program. The Gemini spacecraft
carried two hydrogen-oxygen fuel cell battery sections like this one adapter/equipment
section.
Technical Details
Each battery section contains three stacks of fuel cells with plumbing. The
stacks are connected in parallel and can be switched in and out of use
individually. Each stack has 32 individual cells connected in series and
produces about 490 amperes at 23 to 26 volts. Maximum power output per
battery section is about kilowatt.
The Gemini fuel cell consists of a thin, water-saturated plastic membrane 0.25
millimeters (0.01 inches) thick sandwiched between two thin sheets of platinum
which act as electrodes. The plastic molecules in the membrane have mobile
hydrogen ions lightly bound to them. Both the membrane and the platinum
participate in the reaction. Each electrode forms a wall of a gas chamber.
When a hydrogen gas molecule (H2) comes in contact with its electrode (anode),
the platinum catalyzes it to two hydrogen ions (2H+) and two electrons (2e-).
On the other side, oxygen gas is catalyzed to two oxygen ions (2O-), which can
combine with the hydrogen ions in the membrane to form water (H2O). This
leaves the oxygen electrode (cathode) with a positive charge. If the two
electrodes are connected, the electrons from the anode are drawn to the
cathode, forming a usable electric current. Meanwhile, the hydrogen ions at
the anode enter the membrane to replace the ions removed at the cathode to
form water. Because of this transfer of ions across the membrane, the Gemini
cell is called an Ion Exchange Membrane type cell. The Gemini fuel cell is
built by the General Electric Corporation.