GB756135A - Improvements in missile carrying aircraft - Google Patents
Improvements in missile carrying aircraftInfo
- Publication number
- GB756135A GB756135A GB33247/54A GB3324754A GB756135A GB 756135 A GB756135 A GB 756135A GB 33247/54 A GB33247/54 A GB 33247/54A GB 3324754 A GB3324754 A GB 3324754A GB 756135 A GB756135 A GB 756135A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missile
- aircraft
- energy
- wing
- propelling means
- 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.)
- Expired
Links
- 239000002828 fuel tank Substances 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
756,135. Aircraft. ZBOROWSKI, H. P. G. A. R. VON. Nov. 17, 1954 [Nov. 19, 1953], No. 33247/54. Class 4. [Also in Group XXI] An aircraft provided with means for carrying and launching at least one missile, the aircraft and missile each having propelling means and a source of energy therefor, is characterized by means for connecting the missile propelling means with the aircraft source of energy, whereby, while the missile is carried by the aircraft, the missile propelling means may co-operate in the aircraft propulsion without consuming energy from the missile energy source. In Fig. 12, a pipe P detachably corrects the missile propelling means, e.g. a ram jet, with an aircraft fuel tank T. The missile 2 may be constructed according to French Specification 1,033,590, the fuel tanks T<SP>1</SP> thereof being in an annular wing. The aircraft may be as described in Specification 730,069, in which case two missiles may be carried in diametrically opposite positions inside or outside the annular wing. Illustrations are given of conventional aircraft carrying a missile at each wing tip, or one or two slung below the fuselage, or two beneath each wing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR756135X | 1953-11-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB756135A true GB756135A (en) | 1956-08-29 |
Family
ID=9165425
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB33247/54A Expired GB756135A (en) | 1953-11-19 | 1954-11-17 | Improvements in missile carrying aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB756135A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3075728A (en) * | 1959-07-02 | 1963-01-29 | Kogan Alexandre | Jet airplane engine mounting |
-
1954
- 1954-11-17 GB GB33247/54A patent/GB756135A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3075728A (en) * | 1959-07-02 | 1963-01-29 | Kogan Alexandre | Jet airplane engine mounting |
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