A_EMA 66 BD BR_INGLES SA.cdr

Transcription

A_EMA 66 BD BR_INGLES SA.cdr
air systems
EMA 66 BD Br
70 mm Air to Ground Rocket
specifications
EMA 66 BD Br Rocket Motor
External diameter
Length of the motor-rocket
Weight of the motor-rocket
Thrust
Burn time
Rotation
Operating temperatures
70 mm
1059 mm
6,25 kg
5900 N
1.1 s
35 rps
-45 ºC to + 65 ºC
CAB AP HE 70 mm Warhead
Type
Length
Weight
High explosive
396 mm
3.7 kg
CAB AP HE 70 mm Practice Warhead
Type
Lenght
Mass
Aluminium
350 mm
2.4 kg
EOM FAP M28 Fuse
Type
Length
Weight
Diameter
Mechanical
102 mm
0.311 kg
45 mm
The EMA 66 BD Br rockets, of similar use to the MK66, are
double based solid propellant rockets, aerodynamically
stabilized by 3 wrap-around retractable fins for use in
tactical and training operations, against surface targets,
able to be launched from fixed wing or rotative winged
aircraft, by means of conventional launchers for 70 mm
rockets.
In relation to the EMA 40 BD Br rocket, the EMA 66 BD Br is
much longer and has greater thrust and rotation, factors that
give greater stability and precision in the trajectory. Due to
the greater thrust, the rocket has a maximum range of more
than 8 000 meters.
The EMA 66 BD Br rockets can be configured with 70 mm
CAB AP HE warheads and 70 mm CAB TR practice heads.
The rockets equipped with warheads also use EOM FAP
M28 fuses.
ARES Aeroespacial e Defesa S.A.
Estrada São Mateus, 293 - Jd. Primavera - 25.215-283 - Duque de Caxias - RJ - Brazil
Phone: + 55 21 2677 5350 - Fax: + 55 21 2676 1223 - [email protected] - www.ares.ind.br