Title:
【発明の名称】空中飛翔体
Document Type and Number:
Japanese Patent JP2954948
Kind Code:
B2
Abstract:
- Airborne vehicle (1) comprising at least one temporary releasable propulsion unit (2) connected to the rest (3) of said vehicle by means of a fit (4, 7-5,8-9, 10) capable of allowing said propulsion unit to slide parallel to its axis in the opposite direction to the rest (3) of the vehicle.
- According to the invention, this vehicle is notable in that communication (17) is established between, on the one hand, the space (16) located within said fit and arranged between the front of said propulsion unit and said rest (3) of the vehicle and, on the other hand, the aerodynamic flow around said vehicle (1).
- The natural separation of said propulsion unit (2) from the rest (3) of said missile (1).
Inventors:
JANNMARII DEYUPYUI
Application Number:
JP6943589A
Publication Date:
September 27, 1999
Filing Date:
March 23, 1989
Export Citation:
Assignee:
AEROSUPASHIARU SOC NASHONARU IND
International Classes:
B64G1/64; F42B15/36; (IPC1-7): F42B15/36; B64G1/64
Other References:
【文献】米国特許4625649(US,A)
【文献】CANADIAN PATENT OFFICE RECORD(March 24.1959)P2744~P2745
【文献】CANADIAN PATENT OFFICE RECORD(March 24.1959)P2744~P2745
Attorney, Agent or Firm:
Mitsuteru Soga (3 outside)