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FI (list display)

  • F02K9/00
    		•  Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof [1, 3, 2006.01] HB CC 3G106
  • F02K9/08
    		•  .using solid propellants (F02K 9/72 takes precedence; using semi-solid or pulverulent propellants F02K 9/70) [3] HB CC 3G106
  • F02K9/10
    		•  ..Shape or structure of solid propellant charges [3] HB CC 3G106
  • F02K9/12
    		•  ...made of two or more portions burning at different rates [3] HB CC 3G106
  • F02K9/14
    		•  ...made from sheet-like materials, e.g. of carpet-roll type, of layered structure [3] HB CC 3G106
  • F02K9/16
    		•  ...of honeycomb structure [3] HB CC 3G106
  • F02K9/18
    		•  ...of the internal-burning type having a star or like shaped internal cavity [3] HB CC 3G106
  • F02K9/20
    		•  ...of the external-burning type [3] HB CC 3G106
  • F02K9/22
    		•  ...of the front-burning type [3] HB CC 3G106
  • F02K9/24
    		•  ..Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges [3] HB CC 3G106
  • F02K9/26
    		•  ..Burning control [3] HB CC 3G106
  • F02K9/28
    		•  ..having two or more propellant charges with the propulsion gases exhausting through a common nozzle [3] HB CC 3G106
  • F02K9/30
    		•  ..with the propulsion gases exhausting through a plurality of nozzles [3] HB CC 3G106
  • F02K9/32
    		•  ..Constructional parts; Details not otherwise provided for [3, 2006.01] HB CC 3G106
  • F02K9/34
    		•  ...Casings; Combustion chambers; Liners thereof [3] HB CC 3G106
  • F02K9/36
    		•  ...Propellant charge supports [3] HB CC 3G106
  • F02K9/38
    		•  ...Safety devices, e.g. to prevent accidental ignition [3] HB CC 3G106
  • F02K9/40
    		•  ...Cooling arrangements [3] HB CC 3G106
  • F02K9/42
    		•  .using liquid or gaseous propellants (F02K 9/72 takes precedence) [3] HB CC 3G106
  • F02K9/44
    		•  ..Feeding propellants [3] HB CC 3G106
  • F02K9/46
    		•  ...using pumps [3, 2006.01] HB CC 3G106
  • F02K9/48
    		•  ....driven by a gas turbine fed by propellant combustion gases [3] HB CC 3G106
  • F02K9/50
    		•  ...using pressurised fluid to pressurize the propellants [3] HB CC 3G106
  • F02K9/52
    		•  ...Injectors [3, 2006.01] HB CC 3G106
  • F02K9/54
    		•  ...Leakage detectors; Purging systems; Filtration systems [3, 2006.01] HB CC 3G106
  • F02K9/56
    		•  ...Control [3] HB CC 3G106
  • F02K9/58
    		•  ....Propellant feed valves [3, 2006.01] HB CC 3G106
  • F02K9/60
    		•  ..Constructional parts; Details not otherwise provided for [3, 2006.01] HB CC 3G106
  • F02K9/62
    		•  ...Combustion or thrust chambers [3] HB CC 3G106
  • F02K9/64
    		•  ....having cooling arrangements [3] HB CC 3G106
  • F02K9/66
    		•  ....of the rotary type [3] HB CC 3G106
  • F02K9/68
    		•  ...Decomposition chambers [3] HB CC 3G106
  • F02K9/70
    		•  .using semi-solid or pulverulent propellants [3] HB CC 3G106
  • F02K9/72
    		•  .using liquid and solid propellants, i.e. hybrid rocketengine plants [3, 2006.01] HB CC 3G106
  • F02K9/74
    		•  .combined with another jet-propulsion plant [3] HB CC 3G106
  • F02K9/76
    		•  ..combined with another jet-propulsion plant [3, 2006.01] HB CC 3G106
  • F02K9/78
    		•  ..with an air-breathing jet-propulsion plant (with a ram-jet engine F02K 7/18) [3] HB CC 3G106
  • F02K9/80
    		•  .characterised by thrust or thrust vector control (burning control of solid propellants F02K 9/26; feeding control of liquid or gaseous propellants F02K 9/56; re-ignitable, restartable or intermittently operated rocket-engine plants F02K 9/94) [3, 2006.01] HB CC 3G106
  • F02K9/82
    		•  ..by injection of a secondary fluid into the rocket exhaust gases [3] HB CC 3G106
  • F02K9/84
    		•  ..using movable nozzles [3] HB CC 3G106
  • F02K9/86
    		•  ..using nozzle throats of adjustable cross-section [3] HB CC 3G106
  • F02K9/88
    		•  ..using auxiliary rocket nozzles [3] HB CC 3G106
  • F02K9/90
    		•  ..using deflectors (F02K 9/82 takes precedence) [3] HB CC 3G106
  • F02K9/92
    		•  ..incorporating means for reversing or terminating thrust [3] HB CC 3G106
  • F02K9/94
    		•  .Re-ignitable or restartable rocket-engine plants; Intermittently operated rocket-engine plants [3, 2006.01] HB CC 3G106
  • F02K9/95
    		•  .characterised by starting or ignition means or arrangements (safety devices F02K 9/38) [3] HB CC 3G106
  • F02K9/96
    		•  .characterised by specially adapted arrangements for testing or measuring [3] HB CC 3G106
  • F02K9/97
    		•  .Rocket nozzles (thrust or thrust vector control F02K 9/80) [3] HB CC 3G106
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