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IPC Subgroup
F02K 9/8

characterised by thrust or thrust vector control

Introduced: January 1980

Last revised: January 2006

Full Title

Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof > characterised by thrust or thrust vector control

Classification Context

Section:
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Class:
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Subclass:
JET-PROPULSION PLANTS

6 direct subcodes

Child Classifications

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  • F02K 9/82 by injection of a secondary fluid into the rocket exhaust gases
  • F02K 9/84 using movable nozzles
  • F02K 9/86 using nozzle throats of adjustable cross-section
  • F02K 9/88 using auxiliary rocket nozzles
  • F02K 9/9 using deflectors
  • F02K 9/92 incorporating means for reversing or terminating thrust