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  2. Kerosene - Wikipedia

    en.wikipedia.org/wiki/Kerosene

    Kerosene is sometimes used as an additive in diesel fuel to prevent gelling or waxing in cold temperatures. [54] Ultra-low sulfur kerosene is a custom-blended fuel used by the New York City Transit Authority to power its bus fleet.

  3. Cryogenic fuel - Wikipedia

    en.wikipedia.org/wiki/Cryogenic_fuel

    Cryogenic fuels are fuels that require storage at extremely low temperatures in order to maintain them in a liquid state. These fuels are used in machinery that operates in space (e.g. rockets and satellites) where ordinary fuel cannot be used, due to the very low temperatures often encountered in space, and the absence of an environment that supports combustion (on Earth, oxygen is abundant ...

  4. Kerosene heater - Wikipedia

    en.wikipedia.org/wiki/Kerosene_heater

    The Japanese non-vented "fan" heater burns kerosene gas and is known as a gasification type heater. The liquid kerosene fuel is pre-heated via an electric heating element to vaporize the fuel. The resulting gas is collected and forced into the burn chamber where it is ignited and burns with a blue flame, similar to propane.

  5. From electronics to medications, here's a list of things you shouldn't leave in your car as freezing temperatures blast most of the U.S.

  6. RP-1 - Wikipedia

    en.wikipedia.org/wiki/RP-1

    Many early rockets burned kerosene, but as burn times, combustion efficiencies, and combustion-chamber pressures increased, engine masses decreased, which led to unmanageable engine temperatures. Raw kerosene used as coolant tends to dissociate and polymerize. Lightweight products in the form of gas bubbles cause cavitation, and heavy ones in ...

  7. Fire accelerant - Wikipedia

    en.wikipedia.org/wiki/Fire_accelerant

    Fuel oil no. 1, known by various names including kerosene, range oil, coal oil, or Jet-A (aviation) fuel, encompasses a carbon range of C9 to C17. Its flash point ranges between 110 degrees F and 162 degrees F (42 degrees C - 72 degrees C), while its ignition temperature is recorded at 410 degrees F (210 degrees C).

  8. Adiabatic flame temperature - Wikipedia

    en.wikipedia.org/wiki/Adiabatic_flame_temperature

    Assuming initial atmospheric conditions (1 bar and 20 °C), the following table [1] lists the flame temperature for various fuels under constant pressure conditions. The temperatures mentioned here are for a stoichiometric fuel-oxidizer mixture (i.e. equivalence ratio φ = 1).

  9. Burn rate (chemistry) - Wikipedia

    en.wikipedia.org/wiki/Burn_rate_(chemistry)

    Burn rate (typically expressed in mm/s or in/s) is the sample length over time at a given pressure and temperature. For solid fuel propellant, the most common method of measuring burn rate is the Crawford Type Strand Burning Rate Bomb System [ 3 ] (also known as the Crawford Burner or Strand Burner), as described in MIL-STD-286C.