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We can supply small aerial vehicles, piloted by remote radio control or they can follow a  pre-determined navigation plan.

They are useful for on-demand reconnaissance. First-person-view video is streamed back to a ground console, which can be mounted in a vehicle or a backpack.

Vehicles can be made to order. A range of capabilities are available. Five variants have been designed, All can be hand-launched, and do not require a flat runway for recovery. The vehicles are manufactured from fibreglass, and have a very small radar signature.

There are five vehicles in the ORI range, of varying capabilities, sizies, and propulsion types.

This ORI- 1, for example, has the following paramaters:.

  • Wingspan: 1.2 m
  • Payload  0.7 kg
  • Max speed: 100 km/h
  • Max altitude 3.5 km
  • Max flight time 40 min

 

Selection of ORI vehicles

Spacefleet is an agent for Reev River Aerospace, which is the manufacturer.

if you are interested in the ORI, then please get in touch with us at: This email address is being protected from spambots. You need JavaScript enabled to view it.

 

 

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SRM-30 rocket motor

  • Thrust: 340 Newtons
  • Burn time: 0.755 seconds
  • Operating pressure: 62 bar
  • Thrust profile: neutral (within 9-10%)
  • Manufacturing materials: Al casing, steel nozzle/bulkhead
  • Ignition: electric, 2 Amps at 12 Volts
  • FLIGHT TESTED

 

N.B. The performance relates to a low-cost propellant, of Isp ~ 150 seconds. We can easily substitute this for higher-performance propellants, for extended thrust duration.

The 31 mm motor under test

The motor can be manufactured in different lengths, for burn times other than described above.

A performance certificate issued by ELMEC, Ploiesti, Romania, is available.

 

If you are interested in this motor, please get in touch with us at:This email address is being protected from spambots. You need JavaScript enabled to view it.

 

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 120 mm motor casing with end cap removed

  • Thrust: ~7000 N
  • Burn time: 4.7 seconds
  • Specific impulse - delivered: ~152 s
  • Total impulse: 32900 Ns
  • Maximum propellant load: 22 kg (10  segments )
  • Empty mass: ~20 kg
  • Material: Aerospace-grade steel.
  • Wall thickness: 2.5mm
  • Length (end-cap to end of nozzle): 1.73 m
  • Maximum outer diameter (nozzle and end cap overlap the main body tube): 130 mm
  • Outer diameter of body: 120 mm
  • FLIGHT TESTED

 

120 mm motor under test 

Alternative propellants for Isp up to 230-240 s are possible (not yet tested).

The motor is re-usable

The motor can be manufactured in different lengths, for burn times other than described above.

A performance certificate issued by ELMEC, Ploiesti, Romania, is available.

This motor can perform as O-class or P-class, dependent on the propellant used

It is suitable for high-power amateur rocketry

 

If you are interested in this motor, please get in touch with us at: This email address is being protected from spambots. You need JavaScript enabled to view it.