GB1358085A - Rocket combustion chamber using hypergolic components - Google Patents

Rocket combustion chamber using hypergolic components

Info

Publication number
GB1358085A
GB1358085A GB5183571A GB5183571A GB1358085A GB 1358085 A GB1358085 A GB 1358085A GB 5183571 A GB5183571 A GB 5183571A GB 5183571 A GB5183571 A GB 5183571A GB 1358085 A GB1358085 A GB 1358085A
Authority
GB
United Kingdom
Prior art keywords
propellant
blades
fuel
oxygen
components
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
GB5183571A
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1358085A publication Critical patent/GB1358085A/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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00—Hot gas positive-displacement engine plants
    • 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
    • F02K9/52—Injectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Oxygen, Ozone, And Oxides In General (AREA)
GB5183571A 1970-11-28 1971-11-08 Rocket combustion chamber using hypergolic components Expired GB1358085A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702058583 DE2058583C3 (de) 1970-11-28 1970-11-28 Einrichtung zum Einbringen von hypergolen Treibstoffen in die Brennkammer von Raketentriebwerken

Publications (1)

Publication Number Publication Date
GB1358085A true GB1358085A (en) 1974-06-26

Family

ID=5789345

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5183571A Expired GB1358085A (en) 1970-11-28 1971-11-08 Rocket combustion chamber using hypergolic components

Country Status (4)

Country Link
DE (1) DE2058583C3 (enExample)
FR (1) FR2186609B1 (enExample)
GB (1) GB1358085A (enExample)
IT (1) IT951007B (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1983183A3 (en) * 2007-04-17 2012-07-04 Pratt & Whitney Rocketdyne Inc. Ultra-compact, high-performance aerovortical rocket thruster
CN114455104A (zh) * 2022-04-13 2022-05-10 北京凌空天行科技有限责任公司 一种液体飞行器推进剂贮箱消能器及推进装置

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1626070B1 (de) * 1967-11-20 1970-12-03 Messerschmitt Boelkow Blohm Gasgenerator nach Raketenbauart

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1983183A3 (en) * 2007-04-17 2012-07-04 Pratt & Whitney Rocketdyne Inc. Ultra-compact, high-performance aerovortical rocket thruster
CN114455104A (zh) * 2022-04-13 2022-05-10 北京凌空天行科技有限责任公司 一种液体飞行器推进剂贮箱消能器及推进装置
CN114455104B (zh) * 2022-04-13 2022-07-12 北京凌空天行科技有限责任公司 一种液体飞行器推进剂贮箱消能器及推进装置

Also Published As

Publication number Publication date
DE2058583B2 (de) 1974-07-04
DE2058583C3 (de) 1975-02-20
FR2186609B1 (enExample) 1977-10-21
DE2058583A1 (de) 1973-10-18
IT951007B (it) 1973-06-30
FR2186609A1 (enExample) 1974-01-11

Similar Documents

Publication Publication Date Title
GB1401584A (en) Transportation of liquefied combustible gas by ship
GB1421719A (en) Ramjet powered missiles
GB1104447A (en) Improvements in or relating to rocket motors
GB1358085A (en) Rocket combustion chamber using hypergolic components
GB1140272A (en) Improvements in jet propulsion engine fuel supply systems
GB1233061A (enExample)
GB1404843A (en) Acoustic nozzle
GB1038485A (en) Jet propulsion power plant
GB971776A (en) Improvements in prime movers
GB1143117A (en) Improvements relating to gas burners
FR2232685A1 (en) Fluid drive system for rockets - with pre-combustion chamber to raise oxydator-rich gas mixture, and based on main drive electrical system
GB1046909A (en) Rocket thrust chambers
GB1269123A (en) Detonation apparatus
GB1118078A (en) Composite ramjet/rocket propulsion unit
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
GB1028465A (en) Method of deflecting a hot gas jet passing through a nozzle for carrying out the method
ES422411A1 (es) Perfeccionamientos entoberas supersonicas de onda de cho- que.
GB771896A (en) Rocket motors fuelled by a monopropellant
GB1164656A (en) Rocket Engines
US3714785A (en) Rocket engine nozzle with gas spike
GB785210A (en) Combustion chambers
GB1178723A (en) Improvements in Gas Generators such as Rocket Engines
GB1040183A (en) Improvements in hot gas generators and in particular rocket motors
GB733243A (en) Improvements relating to aircraft
GB768969A (en) Improvements in jet propulsion plant

Legal Events

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