JPS5960057A - ブ−スタ用エンジンのノズル - Google Patents

ブ−スタ用エンジンのノズル

Info

Publication number
JPS5960057A
JPS5960057A JP17210082A JP17210082A JPS5960057A JP S5960057 A JPS5960057 A JP S5960057A JP 17210082 A JP17210082 A JP 17210082A JP 17210082 A JP17210082 A JP 17210082A JP S5960057 A JPS5960057 A JP S5960057A
Authority
JP
Japan
Prior art keywords
nozzle
layer
area ratio
booster engine
seconds
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
JP17210082A
Other languages
English (en)
Japanese (ja)
Other versions
JPS618268B2 (enExample
Inventor
Akio Kan
冠 昭夫
Yoshio Wakamatsu
義男 若松
Kyoichiro Tsugi
都木 恭一郎
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.)
National Aerospace Laboratory of Japan
Original Assignee
National Aerospace Laboratory of Japan
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 National Aerospace Laboratory of Japan filed Critical National Aerospace Laboratory of Japan
Priority to JP17210082A priority Critical patent/JPS5960057A/ja
Publication of JPS5960057A publication Critical patent/JPS5960057A/ja
Publication of JPS618268B2 publication Critical patent/JPS618268B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/974Nozzle- linings; Ablative coatings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
JP17210082A 1982-09-30 1982-09-30 ブ−スタ用エンジンのノズル Granted JPS5960057A (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17210082A JPS5960057A (ja) 1982-09-30 1982-09-30 ブ−スタ用エンジンのノズル

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17210082A JPS5960057A (ja) 1982-09-30 1982-09-30 ブ−スタ用エンジンのノズル

Publications (2)

Publication Number Publication Date
JPS5960057A true JPS5960057A (ja) 1984-04-05
JPS618268B2 JPS618268B2 (enExample) 1986-03-13

Family

ID=15935538

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17210082A Granted JPS5960057A (ja) 1982-09-30 1982-09-30 ブ−スタ用エンジンのノズル

Country Status (1)

Country Link
JP (1) JPS5960057A (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020055625A1 (en) * 2018-09-10 2020-03-19 Raytheon Company Resin transfer molded rocket motor nozzle with adaptive geometry

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020055625A1 (en) * 2018-09-10 2020-03-19 Raytheon Company Resin transfer molded rocket motor nozzle with adaptive geometry

Also Published As

Publication number Publication date
JPS618268B2 (enExample) 1986-03-13

Similar Documents

Publication Publication Date Title
US3702688A (en) Space shuttle vehicle and system
US3138009A (en) Transpiration cooling system
US3091924A (en) Gaseous nozzle boundary
US3064418A (en) Solar rocket with pebble bed heat exchanger
EP0028150B1 (en) Improvements in rocket motors or gas generators
JPS5210869A (en) Thin film forming method
Webster Liquid fueled integral rocket/ramjet technology review
GB2064659A (en) Thrust nozzle
US3253403A (en) Nozzle having ablative coating
US3313488A (en) Rocket thrust chamber
Porzio et al. Experimental study of a confined jet thrust vector control nozzle
US3177811A (en) Composite heat-resistant construction
EP0862688B1 (en) Controlled temperature rocket nozzle
US3101591A (en) Vapor-gas injection thrust vector control system
US3287019A (en) Maneuverable target for anti-missile systems
Purser et al. Exploratory Materials and Missile-nose-shape Tests in a 4,000 Degree F Supersonic Air Jet
Ungar Ablation Thermal Protection Systems: Suitability of ablation systems to thermal protection depends on complex physical and chemical processes.
PAINE Use of lifting re-entry vehicles for synergetic maneuvers.
Drexler Design of a high performance solar sail system.
US3460758A (en) Cooling liners for rocket thrust nozzle
CN1080823C (zh) 控温火箭喷管
Billig Tactical missile design concepts
US3353350A (en) Sump for space vehicles
EP0839925A3 (en) Deposition of a thin film on a substrate using a multi-beam source
JPS63311803A (ja) レド−ム支持体