FIELD: rocket engineering. SUBSTANCE: air-dynamic block of steering drive of guided missile has two conduits. Bodies of steering machines with spaces for pistons, switching gears and controlling electromagnets are placed on opposite sides from axes of control vanes. High-pressure space communicating with air intakes is formed between bodies of steering machines. Low-pressure spaces with release windows are formed in zones housing switching gears and controlling electromagnets. EFFECT: simplified design and enhanced dynamic characteristics. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1997 |
|
RU2124697C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
Authors
Dates
1998-11-10—Published
1997-06-17—Filed