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
Links
- 239000000463 material Substances 0.000 claims abstract description 9
- 238000005299 abrasion Methods 0.000 abstract description 4
- 239000000203 mixture Substances 0.000 abstract description 2
- 229920002379 silicone rubber Polymers 0.000 abstract description 2
- 239000004945 silicone rubber Substances 0.000 abstract description 2
- 239000003082 abrasive agent Substances 0.000 abstract 1
- 239000011521 glass Substances 0.000 abstract 1
- 229920002635 polyurethane Polymers 0.000 abstract 1
- 239000004814 polyurethane Substances 0.000 abstract 1
- 229920000915 polyvinyl chloride Polymers 0.000 abstract 1
- 239000004800 polyvinyl chloride Substances 0.000 abstract 1
- 229910052710 silicon Inorganic materials 0.000 abstract 1
- 239000010703 silicon Substances 0.000 abstract 1
- 238000001816 cooling Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 239000003380 propellant Substances 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 238000002679 ablation Methods 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000000796 flavoring agent Substances 0.000 description 1
- 235000019634 flavors Nutrition 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
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
- F02K9/97—Rocket nozzles
- F02K9/974—Nozzle- 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)
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)
| 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 |
-
1982
- 1982-09-30 JP JP17210082A patent/JPS5960057A/ja active Granted
Cited By (1)
| 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 |