JPH0423599U - - Google Patents
Info
- Publication number
- JPH0423599U JPH0423599U JP6571890U JP6571890U JPH0423599U JP H0423599 U JPH0423599 U JP H0423599U JP 6571890 U JP6571890 U JP 6571890U JP 6571890 U JP6571890 U JP 6571890U JP H0423599 U JPH0423599 U JP H0423599U
- Authority
- JP
- Japan
- Prior art keywords
- refrigerant
- outer plate
- heating surface
- communicating
- ejection holes
- 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
- 239000003507 refrigerant Substances 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 3
- 239000003566 sealing material Substances 0.000 claims description 2
- 239000002826 coolant Substances 0.000 claims 1
- 238000001816 cooling Methods 0.000 claims 1
- 238000002844 melting Methods 0.000 claims 1
- 230000008018 melting Effects 0.000 claims 1
- 238000000034 method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
Landscapes
- Physical Or Chemical Processes And Apparatus (AREA)
- Heat Treatments In General, Especially Conveying And Cooling (AREA)
Description
第１図は本考案を適用した回収型衛星の一例を
示す切断側面図、第２図は本考案の一実施例を示
す詳細断面図、第３図は冷媒の噴出状態を示す詳
細断面図、第４図は冷媒タンクの加圧方式の一例
を示す断面図、第５図は従来装置の一例を示す切
断側面図である。
図中、１は衛星本体、２は落下加熱面、１０は
冷媒タンク、１１は冷媒、１３は外側板、１５は
冷媒通路、１６はジヤケツト、１７は噴出孔、１
８はシール材を示す。
FIG. 1 is a cutaway side view showing an example of a recovery satellite to which the present invention is applied, FIG. 2 is a detailed sectional view showing an embodiment of the present invention, and FIG. 3 is a detailed sectional view showing the refrigerant jetting state. FIG. 4 is a cross-sectional view showing an example of a method of pressurizing a refrigerant tank, and FIG. 5 is a cut-away side view showing an example of a conventional device. In the figure, 1 is the satellite body, 2 is the falling heating surface, 10 is the refrigerant tank, 11 is the refrigerant, 13 is the outer plate, 15 is the refrigerant passage, 16 is the jacket, 17 is the ejection hole, 1
8 indicates a sealing material.
Claims (1)
数の噴出孔を形成すると共に、前記外側板の内側
に、前記噴出孔に連通する冷媒通路を形成するジ
ヤケツトを設け、且つ前記冷媒通路に連通し内部
に冷媒を加圧保持するようにした冷媒タンクを備
え、更に前記落下加熱面に、所要の融点を有して
前記噴出孔を閉塞するシール材を備えたことを特
徴とする回収型衛星の冷却装置。 A plurality of ejection holes opening to the falling heating surface are formed in the outer plate of the satellite main body, and a jacket is provided inside the outer plate to form a refrigerant passage communicating with the ejection holes, and communicating with the coolant passage. and a refrigerant tank configured to pressurize and hold refrigerant therein, and further comprising a sealing material having a required melting point and closing the ejection hole on the falling heating surface. cooling system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6571890U JPH0423599U (en) | 1990-06-21 | 1990-06-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6571890U JPH0423599U (en) | 1990-06-21 | 1990-06-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0423599U true JPH0423599U (en) | 1992-02-26 |
Family
ID=31597795
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6571890U Pending JPH0423599U (en) | 1990-06-21 | 1990-06-21 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0423599U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013023079A (en) * | 2011-07-21 | 2013-02-04 | Sadayuki Amiya | Spaceship |
| JP2017132410A (en) * | 2016-01-29 | 2017-08-03 | 三菱重工業株式会社 | Movable body and cooling method thereof |
| JP2018505099A (en) * | 2015-02-13 | 2018-02-22 | 中国科学院▲寧▼波材料技▲術▼▲与▼工程研究所 | Thermal protection and resistance reduction method and system for ultra-high speed aircraft |
-
1990
- 1990-06-21 JP JP6571890U patent/JPH0423599U/ja active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013023079A (en) * | 2011-07-21 | 2013-02-04 | Sadayuki Amiya | Spaceship |
| JP2018505099A (en) * | 2015-02-13 | 2018-02-22 | 中国科学院▲寧▼波材料技▲術▼▲与▼工程研究所 | Thermal protection and resistance reduction method and system for ultra-high speed aircraft |
| JP2017132410A (en) * | 2016-01-29 | 2017-08-03 | 三菱重工業株式会社 | Movable body and cooling method thereof |
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