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Skylark Nano is a short-range single-stage unguided supersonic rocket, designed for simulating a launch to then be recovered with the use of parachutes. The rocket is powered by solid fuel combustion engines and the vehicle is aerodynamically stabilised through four fins. This means that neither a control system or a thrust vector control system is required, therefore making it a simpler and safer piece of equipment.
skylark nano render


Skylark Nano has attracted its fair share of headlines and articles which has led to enquiries from several universities and students, who have used this research vehicle to collect data on the ambient conditions. Skylark Nano is simple in use during both pre-launch and launch operation.


  • Length 2405 mm
  • Diameter 102 mm
  • Lift-off Mass 13.325 kg
  • Payload Mass Up to 1 kg
  • Propellant HTPB
  • Thrust 1526 N
  • Max Thrust 1825 N
  • ISP 181 s
  • Total Motor Impulse 7579 Ns
  • Total Motor Burn Time 5 s
  • Motor Type Solid Propellent
  • Motor Manufacturer Cesaroni Inc.
  • Motor Designation M-1520BS

flight profile

  • Apogee Altitude 17,103 ft
    (5182 m / 5.182 km)
  • Motor Burn Time 5 s
  • Total flight duration 111 s
  • Maximum Acceleration 14 g
  • Maximum Velocity 491 m/s
    (1767 kmh/M 1.4)
  • Velocity at pad exit 27.2 m/s
    (97.9 kmh)
  • Downrange dispersion 850 m / 0.85 km
    (0.53 miles)
skylark nano flight profile

launch site

If unavailable, Skyrora can provide a mobile telemetry kit that will be deployed on the launch site. There is also the potential for co-investment in equipment to allow for future use at the location. The purpose of this kit is to test key components, which will be reused in the company’s future launch vehicles and includes the following:
  • Telemetry ground station
  • Antenna and antenna mount
  • Control computer (laptop PC), to provide communication with the following onboard system
skylark nano launch pad
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skylark nano render flying
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