FIELD: rocket engineering, guided rockets, various classes and types of rockets with lattice aerodynamic surfaces. SUBSTANCE: proposed rocket is built in agreement with normal aerodynamic configuration and has body housing propulsion plant, systems of guidance and control, four immobile wings and four lattice vanes of control system. Wings and vanes are positioned uniformly on body relative to its longitudinal axis. EFFECT: high maneuvering characteristics of rocket thanks to manufacture of wings, lattice vanes and body of rocket with definite relations of dimensions of these parts. 7 dwg
Title | Year | Author | Number |
---|---|---|---|
ROCKET | 1996 |
|
RU2094748C1 |
"CANARD" AERODYNAMIC CONFIGURATION ROCKET | 1997 |
|
RU2111446C1 |
MISSILE | 2002 |
|
RU2234667C1 |
AIRCRAFT GUIDED MISSILE | 2004 |
|
RU2259536C1 |
ROCKET | 2005 |
|
RU2276321C1 |
ROCKET WITH NORMAL AERODYNAMIC CONFIGURATION | 1995 |
|
RU2085825C1 |
ROCKET | 2004 |
|
RU2270413C1 |
ROCKET WITH COMBINED CONTROL | 1996 |
|
RU2096734C1 |
MISSILE WITH NORMAL AERODYNAMIC CONFIGURATION | 2003 |
|
RU2239780C1 |
LATTICE AERODYNAMIC SURFACE | 1995 |
|
RU2085440C1 |
Authors
Dates
1997-07-27—Published
1995-05-11—Filed