3636710

Information

• Patent Grant
• 3636710

• References
• Source

• Patent Number

  3,636,710

• Date Filed

  Not available

• Date Issued

  Tuesday, January 25, 1972
  53 years ago

• CPC

  • F02K9/97 - Rocket nozzles
  • F02K9/62 - Combustion or thrust chambers
  • F02K9/80 - characterised by thrust or thrust vector control
  • F02K9/95 - characterised by starting or ignition means or arrangements
  • F02K9/972 - Fluid cooling arrangements for nozzles
  • F42B10/668 - Injection of a fluid
  • F05D2240/1281 - Plug nozzles

• US Classifications

  • 060 - Power plants