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This page displays all 「FI」 in main group F41A1/00. |
HB:Handbook | ||||
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CC:Concordance | |||||
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Missile propulsion characterised by the use of explosive or combustible propellant charges (projecting missiles without use of explosive or combustible propellant charge F41B; launching rockets or torpedoes F41F 3/00; missile self-propulsion F42B 15/00) [5] | HB | CC | 2C014 | |
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.Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion [5] | HB | CC | 2C014 | |
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.Missile propulsion using the combustion of a liquid or gaseous fuel, e.g. hypergolic fuel [5] | HB | CC | 2C014 | |
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.Adjusting the range without varying elevation angle or propellant charge data, e.g. by venting a part of the propulsive charge gases, or by adjusting the capacity of the cartridge or combustion chamber [5] | HB | CC | 2C014 | |
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.Recoilless guns, i.e. guns having propulsion means producing no recoil [5] | HB | CC | 2C014 | |
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..a counter projectile being used to balance recoil [5] | HB | CC | 2C014 | |