JPS6210264U - - Google Patents
Info
- Publication number
- JPS6210264U JPS6210264U JP10007985U JP10007985U JPS6210264U JP S6210264 U JPS6210264 U JP S6210264U JP 10007985 U JP10007985 U JP 10007985U JP 10007985 U JP10007985 U JP 10007985U JP S6210264 U JPS6210264 U JP S6210264U
- Authority
- JP
- Japan
- Prior art keywords
- wall member
- heat insulating
- insulating material
- surrounding
- carbon
- 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
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 239000011810 insulating material Substances 0.000 claims description 3
- CREMABGTGYGIQB-UHFFFAOYSA-N carbon carbon Chemical compound C.C CREMABGTGYGIQB-UHFFFAOYSA-N 0.000 claims 1
- 239000011203 carbon fibre reinforced carbon Substances 0.000 claims 1
- 239000002131 composite material Substances 0.000 claims 1
- 239000007788 liquid Substances 0.000 claims 1
Landscapes
- Thermal Insulation (AREA)
Description
第１図、第２図および第３図はそれぞれ本考案
の第１、第２および第３の実施例を示すスラスタ
の要部半截断面図、第４図および第５図はそれぞ
れに従来のスラスタを示す要部半截断面図である
。
２，２２，４２，７２……燃焼室、３，２３，
４３，７３……スラストノズル、５１，６１，８
１……燃焼室の内壁部材、５２，６２，８２……
断熱材、４７，６３，７７……燃焼室の外壁部材
。
1, 2 and 3 are half-cut sectional views of main parts of thrusters showing the first, second and third embodiments of the present invention, respectively, and FIGS. 4 and 5 show conventional thrusters, respectively. FIG. 2, 22, 42, 72... combustion chamber, 3, 23,
43, 73... Thrust nozzle, 51, 61, 8
1... Inner wall member of combustion chamber, 52, 62, 82...
Heat insulating material, 47, 63, 77... Outer wall member of the combustion chamber.
Claims (1)
の内壁部材を包容する断熱材と、更にこの断熱材
を包容する外壁部材とを用いて構成した液体ロケ
ツトエンジンのスラスタ燃焼室。 A thruster combustion chamber for a liquid rocket engine constructed using an inner wall member made of a carbon-carbon composite material, a heat insulating material surrounding the inner wall member, and an outer wall member surrounding the heat insulating material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10007985U JPS6210264U (en) | 1985-07-02 | 1985-07-02 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10007985U JPS6210264U (en) | 1985-07-02 | 1985-07-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6210264U true JPS6210264U (en) | 1987-01-22 |
Family
ID=30969557
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10007985U Pending JPS6210264U (en) | 1985-07-02 | 1985-07-02 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6210264U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005519221A (en) * | 2002-03-04 | 2005-06-30 | エズ スペース トランスポーテイション エスアー | Rocket engine |
-
1985
- 1985-07-02 JP JP10007985U patent/JPS6210264U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005519221A (en) * | 2002-03-04 | 2005-06-30 | エズ スペース トランスポーテイション エスアー | Rocket engine |