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  2. Glow fuel - Wikipedia

    en.wikipedia.org/wiki/Glow_fuel

    Glow fuel is a fuel source used in model engines – generally the same or similar fuels can be used in model airplanes, helicopters, cars and boats. [1] Glow fuel can be burned by very simple two-stroke engines or by more complicated four-stroke engines, and these engines can provide impressive amounts of power for their very small size.

  3. Nitro engine - Wikipedia

    en.wikipedia.org/wiki/Nitro_engine

    A nitro engine generally refers to an engine powered with a fuel that contains some portion (usually between 10% and 40%) of nitromethane mixed with methanol.Nitromethane is a highly combustible substance that is generally only used in very specifically designed engines found in Top Fuel drag racing and in miniature internal combustion engines in radio control, control line and free flight ...

  4. Nitromethane - Wikipedia

    en.wikipedia.org/wiki/Nitromethane

    Nitromethane is used as a fuel in motor racing, particularly drag racing, as well as for radio-controlled model power boats, cars, planes and helicopters. In this context, nitromethane is commonly referred to as "nitro fuel" or simply "nitro", and is the principal ingredient for fuel used in the "Top Fuel" category of drag racing. [14]

  5. Octane rating - Wikipedia

    en.wikipedia.org/wiki/Octane_rating

    This difference between RON and MON is known as the fuel's sensitivity, [9] ... [20] 70 81 [21] "Extra (Super/Plus)" in ... it is 10-20% more expensive as 95 RON fuel ...

  6. Hypergolic propellant - Wikipedia

    en.wikipedia.org/wiki/Hypergolic_propellant

    [8] The only rocket-powered fighter ever deployed was the Messerschmitt Me 163B Komet. The Komet had a HWK 109-509, a rocket motor which consumed methanol/hydrazine as fuel and high test peroxide T-Stoff as oxidizer. The hypergolic rocket motor had the advantage of fast climb and quick-hitting tactics at the cost of being very volatile and ...

  7. Rocket propellant - Wikipedia

    en.wikipedia.org/wiki/Rocket_propellant

    Solid fuel rockets have lower specific impulse, a measure of propellant efficiency, than liquid fuel rockets. As a result, the overall performance of solid upper stages is less than liquid stages even though the solid mass ratios are usually in the .91 to .93 range, as good as or better than most liquid propellant upper stages.

  8. .400/350 Nitro Express - Wikipedia

    en.wikipedia.org/wiki/.400/350_Nitro_Express

    The .400/350 Nitro Express was developed by John Rigby & Co by necking down the .400 Purdey and was introduced in 1899. That same year Rigby approached the engineers at Mauser to make a special Gewehr 98 bolt action to handle this cartridge, its introduction in 1900 was the birth of the magnum length bolt action, paving the way for such cartridges as the .375 H&H and .416 Rigby.

  9. Liquid rocket propellant - Wikipedia

    en.wikipedia.org/wiki/Liquid_rocket_propellant

    Kerosene burns about 20% hotter in absolute temperature than hydrogen. Hydrogen's buoyancy. Since hydrogen is a deep cryogen it boils quickly and rises, due to its very low density as a gas. Even when hydrogen burns, the gaseous H 2 O that is formed has a molecular weight of only 18 AMU compared to 29.9 AMU for air, so it also rises quickly ...

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