Skylark Nano
Skyrora
Skylark Nano is a suborbital launch vehicle designed for research and data collection, featuring simple pre-launch and launch operations.
Key figurescomparable across the catalogue
- Mass
- 13.33 kg
- Payload capacity
- 1 kg
- Total impulse
- 5 N·s
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Diameter
- 0.102 M
- Propellant
- HTPB
- Lift-off mass
- 13.325 KG
- Payload mass
- UP TO 1 KG
- Maximum thrust
- 1 825 N (182.5 KG)
- Thrust
- 1 526 N (152.6 KG)
- Motor type
- SOLID PROPELLANT
- ISP
- 181 s
- Total motor impulse
- 5 s
- Motor manufacturer
- CESARONI INC.
About
The Skylark Nano is a suborbital launch vehicle that has garnered attention from universities and students for its potential as a research platform to collect data on ambient conditions. Its pre-launch and launch operations are designed for simplicity. The vehicle uses HTPB solid propellant and is powered by a motor manufactured by Cesaroni Inc. It has a lift-off mass of 13.325 kg and can carry a payload of up to 1 kg. The maximum thrust is 1825 N, with a sustained thrust of 1526 N. The motor has an ISP of 181 seconds and a total motor impulse of 5 seconds. Skyrora also offers a mobile telemetry kit for launch sites that are unavailable, which includes a telemetry ground station, antenna and mount, and a control computer to communicate with onboard systems. This kit tests key components for future launch vehicles.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.