JPS63168247U - - Google Patents
Info
- Publication number
- JPS63168247U JPS63168247U JP6068287U JP6068287U JPS63168247U JP S63168247 U JPS63168247 U JP S63168247U JP 6068287 U JP6068287 U JP 6068287U JP 6068287 U JP6068287 U JP 6068287U JP S63168247 U JPS63168247 U JP S63168247U
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- booster
- ram rocket
- sustainer
- burnt
- 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
Links
- 239000003380 propellant Substances 0.000 claims description 2
- 239000000567 combustion gas Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
Landscapes
- Testing Of Engines (AREA)
- Toys (AREA)
Description
第１図は本考案に係るノズル構造の一例を示す
断面図、第２図は本考案に係るブースタノズルの
消耗速度を示す図、第３図はブースタ推進時にお
けるラムロケツトの燃焼室圧力を示すグラフ、第
４図はブースタ推進時におけるラムロケツトの推
力を示すグラフ、第５図、第６図はそれぞれ従来
のラムロケツトのノズル構造を示す図である。
２１……モータケース、２２……モータインシ
ユレータ、２３……ブースタ推進薬、２４……ブ
ースタノズル、２５……サステーナノズル。
Fig. 1 is a sectional view showing an example of the nozzle structure according to the present invention, Fig. 2 is a diagram showing the wear rate of the booster nozzle according to the invention, and Fig. 3 is a graph showing the combustion chamber pressure of the ram rocket during booster propulsion. , FIG. 4 is a graph showing the thrust of the ram rocket during booster propulsion, and FIGS. 5 and 6 are diagrams showing the nozzle structure of a conventional ram rocket, respectively. 21...Motor case, 22...Motor insulator, 23...Booster propellant, 24...Booster nozzle, 25...Sustainer nozzle.
Claims (1)
燃焼ガスにより消耗する焼失性部材からなるブー
スタノズルを設けたことを特徴とするラムロケツ
トのノズル構造。 A nozzle structure for a ram rocket, characterized in that a booster nozzle made of a burnt-out member that is consumed by the combustion gas of the booster propellant is provided inside the sustainer nozzle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6068287U JPS63168247U (en) | 1987-04-23 | 1987-04-23 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6068287U JPS63168247U (en) | 1987-04-23 | 1987-04-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63168247U true JPS63168247U (en) | 1988-11-01 |
Family
ID=30893310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6068287U Pending JPS63168247U (en) | 1987-04-23 | 1987-04-23 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63168247U (en) |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57131845A (en) * | 1981-02-06 | 1982-08-14 | Nissan Motor Co Ltd | Ram rocket |
-
1987
- 1987-04-23 JP JP6068287U patent/JPS63168247U/ja active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57131845A (en) * | 1981-02-06 | 1982-08-14 | Nissan Motor Co Ltd | Ram rocket |