JPH0452858B2 - - Google Patents

Info

Publication number
JPH0452858B2
JPH0452858B2 JP24612884A JP24612884A JPH0452858B2 JP H0452858 B2 JPH0452858 B2 JP H0452858B2 JP 24612884 A JP24612884 A JP 24612884A JP 24612884 A JP24612884 A JP 24612884A JP H0452858 B2 JPH0452858 B2 JP H0452858B2
Authority
JP
Japan
Prior art keywords
booster
nozzle
propellant chamber
sustainer
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.)
Expired
Application number
JP24612884A
Other languages
English (en)
Japanese (ja)
Other versions
JPS61126361A (ja
Inventor
Hiromichi Matsumoto
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 JP24612884A priority Critical patent/JPS61126361A/ja
Publication of JPS61126361A publication Critical patent/JPS61126361A/ja
Publication of JPH0452858B2 publication Critical patent/JPH0452858B2/ja
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
    • F02K7/00—Plants 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
    • F02K7/10—Plants 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
    • F02K7/18—Composite ram-jet/rocket engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
JP24612884A 1984-11-22 1984-11-22 ラムロケツト Granted JPS61126361A (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP24612884A JPS61126361A (ja) 1984-11-22 1984-11-22 ラムロケツト

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP24612884A JPS61126361A (ja) 1984-11-22 1984-11-22 ラムロケツト

Publications (2)

Publication Number Publication Date
JPS61126361A JPS61126361A (ja) 1986-06-13
JPH0452858B2 true JPH0452858B2 (enrdf_load_html_response) 1992-08-25

Family

ID=17143894

Family Applications (1)

Application Number Title Priority Date Filing Date
JP24612884A Granted JPS61126361A (ja) 1984-11-22 1984-11-22 ラムロケツト

Country Status (1)

Country Link
JP (1) JPS61126361A (enrdf_load_html_response)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08639Y2 (ja) * 1987-05-28 1996-01-10 防衛庁技術研究本部長 ロケットのノズルクロ−ジャ装置
JPH0515559Y2 (enrdf_load_html_response) * 1987-05-28 1993-04-23
JP2009013944A (ja) * 2007-07-09 2009-01-22 Ihi Aerospace Co Ltd ラムロケット
CN115163336B (zh) * 2022-07-29 2024-08-16 上海宇航系统工程研究所 一种运载火箭固体助推器室压分离控制方法及装置

Also Published As

Publication number Publication date
JPS61126361A (ja) 1986-06-13

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