KR830001581A - Exhaust propulsion vehicle multiple launcher - Google Patents
Exhaust propulsion vehicle multiple launcher Download PDFInfo
- Publication number
- KR830001581A KR830001581A KR1019790002680A KR790002680A KR830001581A KR 830001581 A KR830001581 A KR 830001581A KR 1019790002680 A KR1019790002680 A KR 1019790002680A KR 790002680 A KR790002680 A KR 790002680A KR 830001581 A KR830001581 A KR 830001581A
- Authority
- KR
- South Korea
- Prior art keywords
- exhaust
- launch tube
- propulsion vehicle
- vehicle
- vehicle multiple
- Prior art date
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- Excavating Of Shafts Or Tunnels (AREA)
Abstract
내용 없음No content
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음This content is subject to disclosure, so the full text is not included.
제1도는 하나는 로켓트가 저장된 것을 나타내고 다른 하나는 보지된 제1로켓트를 나타내며 또 다른 발사관들은 여러 상승 단계의 점화된 로켓트를 나타내는, 로켓트가 내장된 다수의 발사관들의 개략측면도.Figure 1 is a schematic side view of a number of launch tubes with built-in rockets, one showing the rocket is stored, the other showing the held first rocket, and the other launching tubes representing the ignited rockets of various ascending stages.
제2도는 본 발명의 취약성 커버의 단부도.Figure 2 is an end view of the fragility cover of the present invention.
제3도는 여러 파열 부분들을 형성하기 위한 발사관의 커버에 설치된 다수의 홈을 나타내는 제2도의 선 3-3에 따른 단면도.FIG. 3 is a cross-sectional view taken along line 3-3 of FIG. 2 showing a plurality of grooves installed in the cover of the launch tube for forming various rupture portions.
제4도, 제5도 및 제6도는 로켓트 배기 구름의 압력 및 직경 증가에 의해 커버가 계속적으로 파열되어 크게 되는 것을 나타내는, 제2도의 유사도 이다.4, 5 and 6 are similar views of FIG. 2, showing that the cover is continuously ruptured and enlarged due to an increase in pressure and diameter of the rocket exhaust cloud.
Claims (2)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1019790002680A KR830001581A (en) | 1979-08-07 | 1979-08-07 | Exhaust propulsion vehicle multiple launcher |
KR2019830005974U KR830001723Y1 (en) | 1979-08-07 | 1983-07-07 | Aft launch tube cover |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1019790002680A KR830001581A (en) | 1979-08-07 | 1979-08-07 | Exhaust propulsion vehicle multiple launcher |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR2019830005974U Division KR830001723Y1 (en) | 1979-08-07 | 1983-07-07 | Aft launch tube cover |
Publications (1)
Publication Number | Publication Date |
---|---|
KR830001581A true KR830001581A (en) | 1983-05-17 |
Family
ID=72896654
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019790002680A KR830001581A (en) | 1979-08-07 | 1979-08-07 | Exhaust propulsion vehicle multiple launcher |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR830001581A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101337536B1 (en) * | 2011-09-05 | 2013-12-06 | 주식회사 현대제이콤 | A device for pressure lose protective firing multi sensor node plurality projectiles with same pressure in the projectile scattering equipment |
-
1979
- 1979-08-07 KR KR1019790002680A patent/KR830001581A/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101337536B1 (en) * | 2011-09-05 | 2013-12-06 | 주식회사 현대제이콤 | A device for pressure lose protective firing multi sensor node plurality projectiles with same pressure in the projectile scattering equipment |
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