GB1377604A - Gas generators for rocket engines - Google Patents

Gas generators for rocket engines

Info

Publication number
GB1377604A
GB1377604A GB3908363A GB3908363A GB1377604A GB 1377604 A GB1377604 A GB 1377604A GB 3908363 A GB3908363 A GB 3908363A GB 3908363 A GB3908363 A GB 3908363A GB 1377604 A GB1377604 A GB 1377604A
Authority
GB
United Kingdom
Prior art keywords
turbine
feed
piston
coolant
chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB3908363A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ministere des Armees
Original Assignee
Ministère de la Défense
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ministère de la Défense filed Critical Ministère de la Défense
Publication of GB1377604A publication Critical patent/GB1377604A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/50—Feeding propellants using pressurised fluid to pressurise the propellants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
GB3908363A 1962-10-08 1963-10-03 Gas generators for rocket engines Expired GB1377604A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR911528A FR1605374A (cs) 1962-10-08 1962-10-08

Publications (1)

Publication Number Publication Date
GB1377604A true GB1377604A (en) 1974-12-18

Family

ID=8788226

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3908363A Expired GB1377604A (en) 1962-10-08 1963-10-03 Gas generators for rocket engines

Country Status (2)

Country Link
FR (1) FR1605374A (cs)
GB (1) GB1377604A (cs)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2287076C1 (ru) * 2005-02-24 2006-11-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Двигательная установка для гиперзвукового летательного аппарата
CN117823297A (zh) * 2023-03-27 2024-04-05 海南太空科技有限公司 一种液体火箭点火方法

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2287076C1 (ru) * 2005-02-24 2006-11-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Двигательная установка для гиперзвукового летательного аппарата
CN117823297A (zh) * 2023-03-27 2024-04-05 海南太空科技有限公司 一种液体火箭点火方法

Also Published As

Publication number Publication date
FR1605374A (cs) 1975-02-28

Similar Documents

Publication Publication Date Title
US2505798A (en) Liquid fuel jet propulsion system
US3328957A (en) Ratio control for closed cycle propulsion systems
US2862482A (en) Internal combustion engine
GB1392675A (en) Reaction propulsion engine and method of operation
GB1051972A (cs)
US2689454A (en) Rocket engine
GB1104447A (en) Improvements in or relating to rocket motors
GB1211841A (en) Fluid propulsion mechanisms for rockets
GB899030A (en) Improvements relating to propellant systems for rockets
GB1138636A (en) Improvements in solid fuel rocket propulsion units
US2838034A (en) Monofuel internal decomposition engine
GB1377604A (en) Gas generators for rocket engines
GB1186375A (en) Improvements in or relating to Engine-Starter Systems including a Self-Contained Air-Compressor feeding a Pneumatic Starter Motor
GB1008157A (en) Improvements in or relating to rocket engines
GB1151579A (en) A Fuel Supply System for Liquid Fuelled Rockets
US3842598A (en) Rocket power plant
GB1320766A (en) Rocket propulsion system
US3147592A (en) Hydrazine gas generator
US2930337A (en) Propulsion motor
GB1118078A (en) Composite ramjet/rocket propulsion unit
US4147025A (en) Formation of auxiliary drive gas for turbine
US3161017A (en) Liquid rocket thrust control
US3345822A (en) Burning rate control of solid propellants
GB1460208A (en) Power plant for an underwater vessel
SU1745001A1 (ru) Жидкостный ракетный двигатель

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee