JPS562448A - Controlling method of thrust for missile - Google Patents

Controlling method of thrust for missile

Info

Publication number
JPS562448A
JPS562448A JP7953279A JP7953279A JPS562448A JP S562448 A JPS562448 A JP S562448A JP 7953279 A JP7953279 A JP 7953279A JP 7953279 A JP7953279 A JP 7953279A JP S562448 A JPS562448 A JP S562448A
Authority
JP
Japan
Prior art keywords
thrust
missile
combustion
propellant
combustion 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.)
Pending
Application number
JP7953279A
Other languages
Japanese (ja)
Inventor
Masayuki Muramatsu
Katsuaki Kosaka
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP7953279A priority Critical patent/JPS562448A/en
Publication of JPS562448A publication Critical patent/JPS562448A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18Composite ram-jet/rocket engines

Abstract

PURPOSE:To control very easily the thrust of a missile to an optional value while the missile is flying, by supplying its propellant of slurry state into the combustion gas of solid propellant while adjusting its supply amount. CONSTITUTION:While a ram rocket 1 is flying, a solid propellant grain 2 is gradually burnt in a primary combustion chamber 6 with the inner face of its inner hole 2a as a combustion face. By this combustion, inflammable combustion gas contg. a large amount of CO, HC and H2 is generated and filled in a primary combustion chamber 6 at high pressure. Then the combustion gas is injected from a nozzle 8 into a secondary combustion chamber 7, mixed with the outside air inducted through a diffuser 9, ignited and then jetted from a tail nozzle 3. At this time, to increase its thrust, a valve 13 is opened to supply the propellant of slurry state in a slurry tank 11 into the inner hole 2a by the pressure of a high pressure source 14, thus to obtain an increase of the thrust.
JP7953279A 1979-06-22 1979-06-22 Controlling method of thrust for missile Pending JPS562448A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7953279A JPS562448A (en) 1979-06-22 1979-06-22 Controlling method of thrust for missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7953279A JPS562448A (en) 1979-06-22 1979-06-22 Controlling method of thrust for missile

Publications (1)

Publication Number Publication Date
JPS562448A true JPS562448A (en) 1981-01-12

Family

ID=13692593

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7953279A Pending JPS562448A (en) 1979-06-22 1979-06-22 Controlling method of thrust for missile

Country Status (1)

Country Link
JP (1) JPS562448A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160021381A (en) * 2014-08-14 2016-02-25 현대로템 주식회사 A Gas flow adjuster

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160021381A (en) * 2014-08-14 2016-02-25 현대로템 주식회사 A Gas flow adjuster

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