Skylark Micro
Skyrora
Skylark Micro is a suborbital launch vehicle designed for testing electrical systems under g-force, evaluating payload material construction and thermal coatings, and launching small satellites for atmospheric research.
Key figurescomparable across the catalogue
- Payload capacity
- 1 kg
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
- Length
- 3.32 m
- Propellant
- HTPB
- Airframe diameter of the first stage
- 0.102 M
- Thrust of the first stage
- 1.56 kN
- Airframe diameter of the second stage
- 0.075 M
- Thrust of the second stage
- 0.84 kN
- Payload mass
- Up to 1 kg
- ISP of the first stage
- 172 s
- Max g-load
- 16
- ISP of the second stage
- 181 s
About
Skylark Micro is a suborbital launch vehicle that facilitates the testing of electrical systems under g-force, utilizing a parachute recovery system for safe landing and payload return. It can also be used to test the construction and thermal coating of payload materials. Additionally, the rocket is capable of launching satellites to investigate ambient conditions in areas of dense atmospheric pressure and serves educational purposes. Skyrora can provide a mobile telemetry kit for launch sites, which includes a telemetry ground station, antenna and antenna mount, and a control computer (laptop PC) to communicate with onboard systems. This kit tests key components of the launch infrastructure for future launch vehicles.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.