CH480614A - Multi-stage rocket with a device for beam control - Google Patents
Multi-stage rocket with a device for beam controlInfo
- Publication number
- CH480614A CH480614A CH857869A CH857869A CH480614A CH 480614 A CH480614 A CH 480614A CH 857869 A CH857869 A CH 857869A CH 857869 A CH857869 A CH 857869A CH 480614 A CH480614 A CH 480614A
- Authority
- CH
- Switzerland
- Prior art keywords
- beam control
- stage rocket
- rocket
- stage
- control
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19681703534 DE1703534C (en) | 1968-06-06 | Missile with mechanically coupled jet and air rudders |
Publications (1)
Publication Number | Publication Date |
---|---|
CH480614A true CH480614A (en) | 1969-10-31 |
Family
ID=5688462
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH857869A CH480614A (en) | 1968-06-06 | 1969-06-05 | Multi-stage rocket with a device for beam control |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH480614A (en) |
FR (1) | FR2010278B1 (en) |
GB (1) | GB1269272A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0227211A1 (en) * | 1985-11-25 | 1987-07-01 | Hughes Aircraft Company | Detachable thrust vector mechanism for an aeronautical vehicle |
DE4300761A1 (en) * | 1993-01-14 | 1994-07-21 | Erno Raumfahrttechnik Gmbh | Control device |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3420441A1 (en) * | 1984-06-01 | 1985-12-05 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | CONTROL DEVICE FOR AIRCRAFT |
-
1969
- 1969-06-03 GB GB2810269A patent/GB1269272A/en not_active Expired
- 1969-06-05 CH CH857869A patent/CH480614A/en not_active IP Right Cessation
- 1969-06-05 FR FR6918588A patent/FR2010278B1/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0227211A1 (en) * | 1985-11-25 | 1987-07-01 | Hughes Aircraft Company | Detachable thrust vector mechanism for an aeronautical vehicle |
DE4300761A1 (en) * | 1993-01-14 | 1994-07-21 | Erno Raumfahrttechnik Gmbh | Control device |
Also Published As
Publication number | Publication date |
---|---|
DE1703534B1 (en) | 1972-07-13 |
FR2010278A1 (en) | 1970-02-13 |
GB1269272A (en) | 1972-04-06 |
FR2010278B1 (en) | 1975-11-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |