FR2266807A1 - Governor for liquid-propelled rocket turbo-pump unit - operated by varying temperature of fuel gas - Google Patents

Governor for liquid-propelled rocket turbo-pump unit - operated by varying temperature of fuel gas

Info

Publication number
FR2266807A1
FR2266807A1 FR7507760A FR7507760A FR2266807A1 FR 2266807 A1 FR2266807 A1 FR 2266807A1 FR 7507760 A FR7507760 A FR 7507760A FR 7507760 A FR7507760 A FR 7507760A FR 2266807 A1 FR2266807 A1 FR 2266807A1
Authority
FR
France
Prior art keywords
fuel
fuel gas
liquid
governor
operated
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.)
Granted
Application number
FR7507760A
Other languages
English (en)
French (fr)
Other versions
FR2266807B1 (ja
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 FR2266807A1 publication Critical patent/FR2266807A1/fr
Application granted granted Critical
Publication of FR2266807B1 publication Critical patent/FR2266807B1/fr
Granted 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
    • F02K9/56—Control
    • F02K9/563—Control of propellant feed pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Turbines (AREA)
FR7507760A 1974-04-03 1975-03-12 Governor for liquid-propelled rocket turbo-pump unit - operated by varying temperature of fuel gas Granted FR2266807A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742416057 DE2416057C3 (de) 1974-04-03 1974-04-03 Verfahren zur Steuerung der oberen und unteren Grenzdrehzahl eines oder mehrerer Turbopumpenaggregate von Flüssigkeitsraketentriebwerken

Publications (2)

Publication Number Publication Date
FR2266807A1 true FR2266807A1 (en) 1975-10-31
FR2266807B1 FR2266807B1 (ja) 1981-12-11

Family

ID=5911975

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7507760A Granted FR2266807A1 (en) 1974-04-03 1975-03-12 Governor for liquid-propelled rocket turbo-pump unit - operated by varying temperature of fuel gas

Country Status (4)

Country Link
JP (1) JPS5849696B2 (ja)
DE (1) DE2416057C3 (ja)
FR (1) FR2266807A1 (ja)
IN (1) IN148684B (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111043042A (zh) * 2019-12-17 2020-04-21 北京深蓝航天科技有限公司 一种液体火箭电动泵装置

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2564671B2 (ja) * 1990-01-16 1996-12-18 均 茎津 空気呼吸型液体ロケット及び液体ロケットの推進剤ポンプ駆動装置
FR2665223B1 (fr) * 1990-07-26 1994-07-08 Snecma Procede pour entrainer simultanement deux pompes a regimes differents et turbopompe pour comprimer simultanement deux fluides.
JP5113230B2 (ja) * 2010-01-04 2013-01-09 貴之 伊東 ロケット発電エンジン及びロケット発電ファンエンジン
US20120204535A1 (en) * 2011-02-15 2012-08-16 Pratt & Whitney Rocketdyne, Inc. Augmented expander cycle

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3577735A (en) * 1969-11-05 1971-05-04 Bolkow Ges Mit Beschrankter Liquid fuel rocket engine construction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111043042A (zh) * 2019-12-17 2020-04-21 北京深蓝航天科技有限公司 一种液体火箭电动泵装置

Also Published As

Publication number Publication date
DE2416057A1 (de) 1975-10-30
DE2416057B2 (de) 1979-10-04
JPS50135417A (ja) 1975-10-27
DE2416057C3 (de) 1980-06-19
IN148684B (ja) 1981-05-09
JPS5849696B2 (ja) 1983-11-05
FR2266807B1 (ja) 1981-12-11

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Legal Events

Date Code Title Description
ST Notification of lapse