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RD-701FFAR 

ROCKET 70MM

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 : 3,000-4,00)M

PLATFORM

  • High speed Aircraft

  • Used by the Indonesian Air Force

  • 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

  • Used by the Indonesian Air Force

  • T-50, F5, F15

India pinaka rocket_edited.jpg

RD-705FFAR

ROCKET 70MM

SPECIFICATION

  • Outside Diameter : 70.5 ± 0.1 mm

  • Overall Length : 1,125 ± 3 mm

  • Screw Thread : 2.400” – 6 – 29o STUB-ACME-3G

  • Weight of the motor rocket : 6.2 ± 0.15 Kg

  • Weight of the propellant : 3.4 ±0.06 kg

  • Type of powder : Double base, extruded, starred central perforation

  • Ignition circuit resistance: 0.70 to 2.00 ohms

  • Ignition current : 28 VDC (1.5-3Amps)

  • Igniter : MK125

  • Burning time: 0.85 ~ 1.3 sec

  • Total Impulse: 7000 ~ 8500 N.sec

  • Max range (G to G) : 12,000M

  • Firing Attack : 6,000- 7,000 M

PLATFORM

  • Low speed Aircraft & Helicopter

  • Used by the Indonesian Army H/C

  • BO-105, H/C Fennec, MI-35P

  • Tactical Vehicle, Surface

  • 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

  • Type of powder : Double base, extruded, starred central perforation

  • 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

  • Burning : 1.0908 sec

  • Average Thrust : 5672 N

  • Total Impulse : 6186 N.sec

  • Stabilization on Trajectory: By linear (Stringht)

  • Launch Spin Rate: About 10rps

  • Estimate Max Range: 10,426m

PLATFORM

  • High speed Aircraft

  • Used by the Indonesian Air Force

  • T-50, F5, F15

  • Non - Hero Safe

ARAS MERCU SDN. BHD.

inquiry@arasmercu.com.my

Lot 36 & 38, Jalan Apollo U5/188, Bandar Pinggiran Subang, 40150 Shah Alam, Selangor

+603-5882 2535 

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