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Specific impulse (abbr. isp) was a measurement for rating the performance of a rocket engine. This measurement gives information on the number of pounds or kilograms of thrust that are derived from the consumption of a pound or kilogram of propellant in one second. The semi-solid propellant moyerite (synthetic) and the hypergolic propellant gronerium compound 3983 had a low specific impulse of 450 isp. These propellants was used in ullage thruster devices and emergency jettison thrusters. (TNG: "Night Terrors" )

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  • Specific impulse
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  • Specific impulse (abbr. isp) was a measurement for rating the performance of a rocket engine. This measurement gives information on the number of pounds or kilograms of thrust that are derived from the consumption of a pound or kilogram of propellant in one second. The semi-solid propellant moyerite (synthetic) and the hypergolic propellant gronerium compound 3983 had a low specific impulse of 450 isp. These propellants was used in ullage thruster devices and emergency jettison thrusters. (TNG: "Night Terrors" )
  • The specific impulse (commonly abbreviated Isp) of a propulsion system is the impulse (change in momentum) per unit of propellant. Depending on whether the amount of propellant is expressed in mass or in weight (by convention weight on the Earth) the dimension of specific impulse is that of speed or time, respectively, differing by a factor of g, the gravitational acceleration at the surface of the Earth.
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abstract
  • Specific impulse (abbr. isp) was a measurement for rating the performance of a rocket engine. This measurement gives information on the number of pounds or kilograms of thrust that are derived from the consumption of a pound or kilogram of propellant in one second. The semi-solid propellant moyerite (synthetic) and the hypergolic propellant gronerium compound 3983 had a low specific impulse of 450 isp. These propellants was used in ullage thruster devices and emergency jettison thrusters. (TNG: "Night Terrors" )
  • The specific impulse (commonly abbreviated Isp) of a propulsion system is the impulse (change in momentum) per unit of propellant. Depending on whether the amount of propellant is expressed in mass or in weight (by convention weight on the Earth) the dimension of specific impulse is that of speed or time, respectively, differing by a factor of g, the gravitational acceleration at the surface of the Earth.
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