

RD-701FFAR
ROCKET 70MM
SPECIFICATION
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Outside Diameter : 70.866 mm
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Overall Length : 998.64 mm
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Screw Thread : 2.400” – 6 – 29o STUB-ACME-3G
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Weight of the motor rocket : 5.044 ± 0.125 Kg
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Weight of the propellant : 2.994 ± 0.125 kg
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Type of powder : Double base N5, extruded, starred central perforation
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Ignition circuit resistance: 0.70 to 2.00 ohms
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Ignition current : 28 VDC (1.5-3Amps)
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Igniter : MK125- Burning : 1.14-1.8 sec
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Burning time: 3.551,6-5.882,4 N.sec
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Max range (G to G) : 7,000M
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Firing Attack : 3,000-4,00)M
PLATFORM
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High speed Aircraft
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Used by the Indonesian Air Force
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T-50, F5, F15
RD-7010FFAR
SPECIFICATION
-
Outside Diameter : 70.866 mm
-
Overall Length : 998.64 mm
-
Screw Thread : 2.400” – 6 – 29o STUB-ACME-3G
-
Weight of the motor rocket : 5.044 ± 0.125 Kg
-
Weight of the propellant : 2.994 ± 0.125 kg
-
Type of powder : Double base N5, extruded, starred central perforation
-
Ignition circuit resistance: 0.70 to 2.00 ohms
-
Ignition current : 28 VDC (1.5-3Amps)
-
Igniter : MK125
-
Burning : 1.14-1.8 sec
-
Burning time: 3.551,6-5.882,4 N.sec
-
Max range (G to G) : 7,000M
-
Firing Attack : 3,000-4,000M
PLATFORM
-
High speed Aircraft
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Used by the Indonesian Air Force
-
T-50, F5, F15

RD-705FFAR
ROCKET 70MM
SPECIFICATION
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Outside Diameter : 70.5 ± 0.1 mm
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Overall Length : 1,125 ± 3 mm
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Screw Thread : 2.400” – 6 – 29o STUB-ACME-3G
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Weight of the motor rocket : 6.2 ± 0.15 Kg
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Weight of the propellant : 3.4 ±0.06 kg
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Type of powder : Double base, extruded, starred central perforation
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Ignition circuit resistance: 0.70 to 2.00 ohms
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Ignition current : 28 VDC (1.5-3Amps)
-
Igniter : MK125
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Burning time: 0.85 ~ 1.3 sec
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Total Impulse: 7000 ~ 8500 N.sec
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Max range (G to G) : 12,000M
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Firing Attack : 6,000- 7,000 M
PLATFORM
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Low speed Aircraft & Helicopter
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Used by the Indonesian Army H/C
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BO-105, H/C Fennec, MI-35P
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Tactical Vehicle, Surface
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Non-Hero Safe

RD-7010FFAR
SPECIFICATION
-
Outside Diameter : 70.866 mm
-
Overall Length : 1.126,7 mm
-
Screw Thread : 2.400” – 6 – 29o STUB-ACME-3G (corresponding with 2,75" warhead)
-
Weight of the motor rocket : 5763 ± 0.05 kg
-
Weight of the propellant : 3.4 ± 0.06 kg
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Type of powder : Double base, extruded, starred central perforation
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Ignition circuit resistance: 0.70 to 2.00 ohms
-
Ignition current : 28 ± 2 VDC
- Recommended : 3 Amps
- Minimum : 1.5 Amp for 10 msec -
Igniter : MK125 MOD.5 or MOD.5 Bg
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Burning : 1.0908 sec
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Average Thrust : 5672 N
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Total Impulse : 6186 N.sec
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Stabilization on Trajectory: By linear (Stringht)
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Launch Spin Rate: About 10rps
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Estimate Max Range: 10,426m
PLATFORM
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High speed Aircraft
-
Used by the Indonesian Air Force
-
T-50, F5, F15
-
Non - Hero Safe
