GB1352479A – Rocket engine
– Google Patents
GB1352479A – Rocket engine
– Google Patents
Rocket engine
Info
Publication number
GB1352479A
GB1352479A
GB2305372A
GB2305372A
GB1352479A
GB 1352479 A
GB1352479 A
GB 1352479A
GB 2305372 A
GB2305372 A
GB 2305372A
GB 2305372 A
GB2305372 A
GB 2305372A
GB 1352479 A
GB1352479 A
GB 1352479A
Authority
GB
United Kingdom
Prior art keywords
charge
nozzle
rocket engine
combustion chamber
insulating material
Prior art date
1971-05-27
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
GB2305372A
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.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle 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.)
1971-05-27
Filing date
1972-05-17
Publication date
1974-05-08
1972-05-17
Application filed by Werkzeugmaschinenfabrik Oerlikon Buhrle AG
filed
Critical
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
1974-05-08
Publication of GB1352479A
publication
Critical
patent/GB1352479A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
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
F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
F02K9/32—Constructional parts; Details not otherwise provided for
F02K9/34—Casings; Combustion chambers; Liners thereof
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
F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
F02K9/10—Shape or structure of solid propellant charges
F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
Abstract
1352479 Rocket engines WERKZEUGMASCHINENFABRIK OERLIKONBUHRLE AG 17 May 1972 [27 May 1971] 23053/72 Heading F3A A rocket engine comprises a nozzle 19 carried by a member 8 which is attached to a projection 5 extending from the floor 3 of the combustion chamber 1. The nozzle is supported on the shoulder 20 of a steel sleeve 16 containing an inner sleeve 22 of thermally insulating material. The combustion chamber 1 is made of aluminium alloy and is lined with thermally insulating material. The propellant charge 2 is ignitable by means 7 and consists of a launching charge 2a of large surface area and a cruising charge 2b. The member 8 is formed of fibre reinforced phenolic resin.
GB2305372A
1971-05-27
1972-05-17
Rocket engine
Expired
GB1352479A
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
CH775371A
CH539200A
(en)
1971-05-27
1971-05-27
Rocket engine
Publications (1)
Publication Number
Publication Date
GB1352479A
true
GB1352479A
(en)
1974-05-08
Family
ID=4329960
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB2305372A
Expired
GB1352479A
(en)
1971-05-27
1972-05-17
Rocket engine
Country Status (9)
Country
Link
US
(1)
US3779012A
(en)
BE
(1)
BE783806A
(en)
CH
(1)
CH539200A
(en)
DE
(1)
DE2221162C3
(en)
FR
(1)
FR2138691B1
(en)
GB
(1)
GB1352479A
(en)
IL
(1)
IL39523A
(en)
IT
(1)
IT955744B
(en)
SE
(1)
SE379398B
(en)
Families Citing this family (3)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US5101731A
(en)
*
1990-11-30
1992-04-07
The United States Of America As Represented By The Secretary Of The Navy
Propellant grain assembly for a gas generator
RU2490499C1
(en)
*
2012-04-09
2013-08-20
Открытое акционерное общество «Научно-исследовательский институт полимерных материалов»
Solid-propellant charge
US8975565B2
(en)
*
2012-07-17
2015-03-10
Raytheon Company
Integrated propulsion and attitude control system from a common pressure vessel for an interceptor
Family Cites Families (5)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US2944389A
(en)
*
1944-11-20
1960-07-12
Clarence E Weinland
Rotating rocket motor and method of making same
US3165889A
(en)
*
1958-11-24
1965-01-19
Richard B Kershner
Jet control by rotatable offset nozzle
US3151449A
(en)
*
1961-08-25
1964-10-06
Curtiss Wright Corp
Rocket nozzle cooling system
US3147591A
(en)
*
1961-12-28
1964-09-08
Gen Motors Corp
Swiveling fluid jet exhaust nozzle construction
US3520139A
(en)
*
1964-06-11
1970-07-14
Curtiss Wright Corp
Nozzle coolant supply system
1971
1971-05-27
CH
CH775371A
patent/CH539200A/en
not_active
IP Right Cessation
1972
1972-04-28
DE
DE2221162A
patent/DE2221162C3/en
not_active
Expired
1972-05-05
SE
SE7206008A
patent/SE379398B/xx
unknown
1972-05-12
FR
FR7216946A
patent/FR2138691B1/fr
not_active
Expired
1972-05-17
GB
GB2305372A
patent/GB1352479A/en
not_active
Expired
1972-05-17
US
US00254083A
patent/US3779012A/en
not_active
Expired – Lifetime
1972-05-23
BE
BE783806A
patent/BE783806A/en
unknown
1972-05-23
IT
IT24693/72A
patent/IT955744B/en
active
1972-05-24
IL
IL39523A
patent/IL39523A/en
unknown
Also Published As
Publication number
Publication date
FR2138691A1
(en)
1973-01-05
DE2221162C3
(en)
1974-08-22
IL39523A
(en)
1974-07-31
DE2221162B2
(en)
1974-01-31
CH539200A
(en)
1973-07-15
IT955744B
(en)
1973-09-29
SE379398B
(en)
1975-10-06
IL39523A0
(en)
1972-10-29
US3779012A
(en)
1973-12-18
DE2221162A1
(en)
1972-11-30
BE783806A
(en)
1972-09-18
FR2138691B1
(en)
1975-03-21
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Legal Events
Date
Code
Title
Description
1974-09-18
PS
Patent sealed [section 19, patents act 1949]
1982-12-15
PCNP
Patent ceased through non-payment of renewal fee
