JPS5612036A - End face combustion type rocket motor - Google Patents

End face combustion type rocket motor

Info

Publication number
JPS5612036A
JPS5612036A JP8793279A JP8793279A JPS5612036A JP S5612036 A JPS5612036 A JP S5612036A JP 8793279 A JP8793279 A JP 8793279A JP 8793279 A JP8793279 A JP 8793279A JP S5612036 A JPS5612036 A JP S5612036A
Authority
JP
Japan
Prior art keywords
rocket motor
combustion type
restrictor
type rocket
loading
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
JP8793279A
Other languages
Japanese (ja)
Inventor
Takemasa Koreki
Takayoshi Fuji
Toshinobu Ochiai
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 JP8793279A priority Critical patent/JPS5612036A/en
Publication of JPS5612036A publication Critical patent/JPS5612036A/en
Pending legal-status Critical Current

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Abstract

PURPOSE: To obtain stable combustion performance by loading the composite double base propellant grain, which is coated by a restrictor with specific hardness, using the free standing method.
CONSTITUTION: For example, a rocket motor is constituted by loading in a motor chamber 1 in accordance with the free standing method a mixture of 80wt% of a double base system component consisting of 50.0wt% of nitrocellulose, 41.0wt% of nitroglycerine and 9.0wt% of ethylcentralit, 15wt% of ammonium perchlorate, and 5wt% of RDX on which mixture a restrictor 10 with a Shore hardness A of 70 or more.
COPYRIGHT: (C)1981,JPO&Japio
JP8793279A 1979-07-10 1979-07-10 End face combustion type rocket motor Pending JPS5612036A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8793279A JPS5612036A (en) 1979-07-10 1979-07-10 End face combustion type rocket motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8793279A JPS5612036A (en) 1979-07-10 1979-07-10 End face combustion type rocket motor

Publications (1)

Publication Number Publication Date
JPS5612036A true JPS5612036A (en) 1981-02-05

Family

ID=13928675

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8793279A Pending JPS5612036A (en) 1979-07-10 1979-07-10 End face combustion type rocket motor

Country Status (1)

Country Link
JP (1) JPS5612036A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59143653A (en) * 1983-02-05 1984-08-17 Konishiroku Photo Ind Co Ltd Liquid discharge apparatus
JPS59143654A (en) * 1983-02-05 1984-08-17 Konishiroku Photo Ind Co Ltd Liquid discharge apparatus
US5541633A (en) * 1992-02-12 1996-07-30 Xerox Corporation Ink jet printing of concealed images on carbonless paper

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59143653A (en) * 1983-02-05 1984-08-17 Konishiroku Photo Ind Co Ltd Liquid discharge apparatus
JPS59143654A (en) * 1983-02-05 1984-08-17 Konishiroku Photo Ind Co Ltd Liquid discharge apparatus
JPH0330507B2 (en) * 1983-02-05 1991-04-30
JPH0330503B2 (en) * 1983-02-05 1991-04-30
US5541633A (en) * 1992-02-12 1996-07-30 Xerox Corporation Ink jet printing of concealed images on carbonless paper

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