JPH0332158U - - Google Patents
Info
- Publication number
- JPH0332158U JPH0332158U JP9272889U JP9272889U JPH0332158U JP H0332158 U JPH0332158 U JP H0332158U JP 9272889 U JP9272889 U JP 9272889U JP 9272889 U JP9272889 U JP 9272889U JP H0332158 U JPH0332158 U JP H0332158U
- Authority
- JP
- Japan
- Prior art keywords
- stage
- combustion chamber
- bulkhead
- stage combustion
- propellant
- 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 6
- 239000003380 propellant Substances 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims 2
- 239000010959 steel Substances 0.000 claims 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims 1
Landscapes
- Excavating Of Shafts Or Tunnels (AREA)
Description
第1図はこの考案の一実施例による2段推力推
進用圧力隔壁装置を示す断面図、第2図は、その
実施例の作動を示す断面図、第3図はこの考案の
飛しよう体への応用を示す断面図、第4図は従来
の2段推力推進用圧力隔壁装置を示す断面図であ
る。
図において、1…第1段燃焼室、2…第2段燃
焼室、3…第1段推進薬、4…第2段推進薬、5
…分離型隔壁、6…第1段点火器である。なお、
図中、同一符号は同一、又は相当部分を示す。
Fig. 1 is a sectional view showing a two-stage thrust propulsion pressure bulkhead device according to an embodiment of this invention, Fig. 2 is a sectional view showing the operation of the embodiment, and Fig. 3 is a sectional view showing a pressure bulkhead device for two-stage thrust propulsion according to an embodiment of this invention. FIG. 4 is a sectional view showing a conventional pressure bulkhead device for two-stage thrust propulsion. In the figure, 1...first stage combustion chamber, 2...second stage combustion chamber, 3...first stage propellant, 4...second stage propellant, 5
... Separate bulkhead, 6... First stage igniter. In addition,
In the figures, the same reference numerals indicate the same or corresponding parts.
Claims (1)
焼室とこの第1段燃焼室内に充填された第1段推
進薬及び点火器、同じく第2段燃焼室と推進薬、
この第2段燃焼室に鋼材台座を介して固定された
焼尽性隔壁又、この焼尽性隔壁にO−リングを通
して取り付けられた鋼材隔壁及び断熱シールを備
えた事を特徴とする2段推力推進用圧力隔壁。 In a propulsion machine that generates two-stage thrust, a first-stage combustion chamber, a first-stage propellant and an igniter filled in the first-stage combustion chamber, a second-stage combustion chamber and a propellant,
A two-stage thrust propulsion system characterized by comprising an exhaustible bulkhead fixed to the second stage combustion chamber via a steel pedestal, a steel bulkhead and a heat insulating seal attached to the burnable bulkhead through an O-ring. pressure bulkhead.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9272889U JPH0332158U (en) | 1989-08-07 | 1989-08-07 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9272889U JPH0332158U (en) | 1989-08-07 | 1989-08-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0332158U true JPH0332158U (en) | 1991-03-28 |
Family
ID=31642139
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9272889U Pending JPH0332158U (en) | 1989-08-07 | 1989-08-07 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0332158U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001220283A (en) * | 2000-02-09 | 2001-08-14 | Daicel Chem Ind Ltd | Combustor |
JP2009013944A (en) * | 2007-07-09 | 2009-01-22 | Ihi Aerospace Co Ltd | Ram rocket |
JP2011237075A (en) * | 2010-05-07 | 2011-11-24 | Mitsubishi Heavy Ind Ltd | Flying object |
-
1989
- 1989-08-07 JP JP9272889U patent/JPH0332158U/ja active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001220283A (en) * | 2000-02-09 | 2001-08-14 | Daicel Chem Ind Ltd | Combustor |
JP2009013944A (en) * | 2007-07-09 | 2009-01-22 | Ihi Aerospace Co Ltd | Ram rocket |
JP2011237075A (en) * | 2010-05-07 | 2011-11-24 | Mitsubishi Heavy Ind Ltd | Flying object |