Function | Medium-lift launch vehicle |
---|---|
Manufacturer | Stoke Space |
Country of origin | United States |
Size | |
Height | 40.2 m (132 ft) |
Diameter | 4.2 m (14 ft) |
Mass | 227,000 kg (500,000 lb) |
Stages | 2 |
Associated rockets | |
Comparable | |
First stage | |
Height | 27.1 m (89 ft) |
Diameter | 3.81 m (12.5 ft) |
Propellant mass | 183,705 kg (405,000 lb)[1] |
Powered by | 7 × S1E |
Maximum thrust |
|
Specific impulse |
|
Propellant | CH4 / LOX |
Second stage | |
Height | 13.1 m (43 ft) |
Diameter | 4.2 m (14 ft) |
Propellant mass | 18,000 kg (40,000 lb) |
Powered by | 1 x S2E |
Maximum thrust | 111 kN (25,000 lbf) |
Specific impulse | 430 s (4.2 km/s) [2] |
Propellant | LH2 / LOX |
Launch history | |
Status | In development |
Launch sites | Cape Canaveral LC-14 |
Total launches | 0 |
Nova is a fully reusable medium-lift launch vehicle being developed by Stoke Space.[3] Announced in October 2023,[4] Stoke Space plans to use two stages with an expected payload capacity of 5 tons (5,000 kg) to low Earth orbit (LEO), with the first stage performing a return-to-launch-site (RTLS) landing. The company plans to use 7 conventional full-flow staged combustion rocket engines, burning methalox. The second stage will use a hydrolox (liquid hydrogen/liquid oxygen) engine with 30 thrust chambers ringing a regeneratively cooled heatshield,[5] eliminating the need for thermal tiles.[6][7] A center passive bleed in the second stage aims to create an aerospike engine-like effect for improved efficiency.
The vehicle was selected as part of the Space Force's Orbital Services Program.[8]