Liquid hydrogen is a common
liquid rocket fuel for
rocketry application and is used by
NASA and the
U.S. Air Force, which operate a large number of liquid hydrogen tanks with an individual capacity up to 3.8 million liters (1 million U.S. gallons). In most
rocket engines fueled by liquid hydrogen, it first
cools the nozzle and other parts before being mixed with the oxidizer, usually
liquid oxygen, and burned to produce water with traces of
ozone and
hydrogen peroxide. Practical H2–O2 rocket engines run fuel-rich so that the exhaust contains some unburned hydrogen. This reduces combustion chamber and nozzle erosion. It also reduces the molecular weight of the exhaust, which can increase
specific impulse, despite the incomplete combustion. Liquid hydrogen can be used as the fuel for an
internal combustion engine or
fuel cell. The
MF Hydra ferry is powered by liquid hydrogen. Various submarines, including the
Type 212 submarine,
Type 214 submarine, and others, and concept
hydrogen vehicles have been built using this form of hydrogen, such as the
DeepC,
BMW H2R, and others. Due to its similarity, builders can sometimes modify and share equipment with systems designed for
liquefied natural gas (LNG). Liquid hydrogen is being investigated as a
zero carbon fuel for
aircraft. Because of the lower
volumetric energy, the hydrogen volumes needed for combustion are large. Unless
direct injection is used, a severe gas-displacement effect also hampers maximum breathing and increases pumping losses. Liquid hydrogen is also used to cool neutrons to be used in
neutron scattering. Since neutrons and hydrogen nuclei have similar masses, kinetic energy exchange per interaction is maximum (
elastic collision). Finally, superheated liquid hydrogen was used in many
bubble chamber experiments. The first
thermonuclear bomb,
Ivy Mike, used liquid
deuterium, also known as hydrogen-2, for nuclear fusion. ==Properties==