JPS59190098A - Space-shuttle in which orbitor, which can be folded and encased, of blade is installed at nose of external fuel tank - Google Patents
Space-shuttle in which orbitor, which can be folded and encased, of blade is installed at nose of external fuel tankInfo
- Publication number
- JPS59190098A JPS59190098A JP6281083A JP6281083A JPS59190098A JP S59190098 A JPS59190098 A JP S59190098A JP 6281083 A JP6281083 A JP 6281083A JP 6281083 A JP6281083 A JP 6281083A JP S59190098 A JPS59190098 A JP S59190098A
- Authority
- JP
- Japan
- Prior art keywords
- fuel tank
- external fuel
- folded
- shuttle
- orbitor
- 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
- 239000002828 fuel tank Substances 0.000 title claims description 7
- 239000000446 fuel Substances 0.000 description 2
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
Landscapes
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
この発明は、外部燃料タンク（３）の先端に収納可能翼
を装着した、オービタ−（１）に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an orbiter (1) equipped with a retractable wing at the tip of an external fuel tank (3).
従来のスペース・シャトルは、発射時、外部燃料タンク
（３）の背に耐着しているため、非常に空気抵抗を受け
ることになるが、本発明は、それらの欠点を除くために
発明されたものでこれを図面について説明すれば、
（イ）外部燃料タンク（３）の先端部にオービタ−（１
）をはめ込んであり、又、その翼（２）が出し入れ自由
の収納式になっているため、大気進行中、ロケット全体
に受ける空気抵抗は非常に減少される故、速度増加、燃
料節約にも大変役立ち本体の性能をアップする事になる
。The conventional space shuttle is attached to the back of the external fuel tank (3) at the time of launch, so it is subject to significant air resistance, but the present invention was invented to eliminate these drawbacks. To explain this with reference to the drawing, (a) there is an orbiter (1) at the tip of the external fuel tank (3).
), and its wings (2) are retractable and can be taken out and put in freely, so the air resistance that the rocket receives as a whole during the atmosphere is greatly reduced, which increases speed and saves fuel. This will be very useful and will improve the performance of the main unit.
本発明は、以上のような構造である。なお、収納翼は、
必要に応じて、出し入れは、自由である。The present invention has the above structure. In addition, the storage wing is
You are free to put in and take out as needed.
第１図は、本発明スペース・シャトルの内部を示した全
体側面図
第２図は、外部燃料タンク等と、オービタ−を各々にし
た側面・部分図
（１）はオービタ−（７）はタービン・ポンプ（２）は
収納可能翼 （８）は燃焼室（３）は外部燃料タ
ンク （９）はノズル（４）はロケット、ブースター
（５）は酸化剤 （１０）はツギ目（６）は
液体燃料 （］１）はオービタ−ノズル特許出
願人 梅 原 武
特開昭５９−１９００９８（２）Figure 1 is an overall side view showing the inside of the space shuttle of the present invention. Figure 2 is a side and partial view showing the external fuel tank, etc. and the orbiter (1). The orbiter (7) is a turbine.・Pump (2) is a retractable wing (8) is a combustion chamber (3) is an external fuel tank (9) is a nozzle (4) is a rocket, booster (5) is an oxidizer (10) is a serpentine (6) is Liquid fuel (]1) is the orbiter nozzle patent applicant Takeshi Umehara Japanese Patent Application Publication No. 1983-190098 (2)
Claims (1)
来る翼（２）を所持している。オービタ−（１）を装着
ｔ、 タスペースーシャトル 以上の如く構成された。先端装備スペース・シャトル[Claims] (a) It has a wing (2) that can be folded and stored at the tip of the external fuel tank (3). It was equipped with an orbiter (1) and was configured more like a Space Shuttle. Advanced Space Shuttle
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6281083A JPS59190098A (en) | 1983-04-09 | 1983-04-09 | Space-shuttle in which orbitor, which can be folded and encased, of blade is installed at nose of external fuel tank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6281083A JPS59190098A (en) | 1983-04-09 | 1983-04-09 | Space-shuttle in which orbitor, which can be folded and encased, of blade is installed at nose of external fuel tank |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS59190098A true JPS59190098A (en) | 1984-10-27 |
Family
ID=13211063
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6281083A Pending JPS59190098A (en) | 1983-04-09 | 1983-04-09 | Space-shuttle in which orbitor, which can be folded and encased, of blade is installed at nose of external fuel tank |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59190098A (en) |
-
1983
- 1983-04-09 JP JP6281083A patent/JPS59190098A/en active Pending
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