Title:
【発明の名称】誘導飛しょう体およびその誘導方法
Document Type and Number:
Japanese Patent JP2912368
Kind Code:
B1
Abstract:
PROBLEM TO BE SOLVED: To assure stably flying by providing an aerodynamic characteristic altering means for moving an aerodynamic center of a guided airframe carried at an aircraft, launched or dropped toward a target, and flown toward rearward rear of an airframe body, and a thrust deflecting means for deflecting a thrust of the body. SOLUTION: A guided airframe 32 launched, dropped or separated from a mother aircraft flying at a speed V0 (e.g. a supersonic speed range) is flown rear of an airframe body toward an advancing direction of a mother aircraft at a speed Vb immediately after separating with a dome 1 rearward and a cover 12 ahead. At the time of flying, static stability is assured by a balance between lift characteristics of a lattice wing 36 and lift characteristic of a fixed wing 35, thereby guaranteeing stable flying. After a predetermined time from the time of separating from the aircraft, a propulsion unit 11 is ignited, a holding member of the cover 12 is removed, the cover 12 is discharged rear of the body, exhaust fumes of the unit are discharged in a direction opposite to a flow of an air stream, and the airframe is flown rearward.
Inventors:
MIHARA SOICHIRO
Application Number:
JP19296898A
Publication Date:
June 28, 1999
Filing Date:
July 08, 1998
Export Citation:
Assignee:
MITSUBISHI DENKI KK
International Classes:
B64C13/18; F42B10/64; F42B10/66; F41G7/20; F42B15/00; G05D1/10; (IPC1-7): F42B15/00; F42B10/64; F42B10/66
Domestic Patent References:
| JP842998A | ||||
| JP579798A | ||||
| JP112500A |
Other References:
【文献】特許2640905(JP,B2)
【文献】特許2807437(JP,B2)
【文献】特許2807437(JP,B2)
Attorney, Agent or Firm:
Kaneo Miyata (2 outside)