Nova

Active Re-Usable

Stoke Space (Stoke)

None

Description

Stoke Space’s Nova launch vehicle is a planned fully reusable 2-stage rocket. The 1st stage uses 7 Zenith Full-flow staged-combustion (FFSC) engines using Liquified natural gas/liquid oxygen (LNG/LOX)​ as fuel, with restartable capability and landing legs for landing. The 2nd stage is unconventionally designed around a 24-thrust chamber liquid hydrogen/liquid oxygen (LH2/LOX) expander cycle rocket engine that surrounds a regeneratively cooled heat shield, thus enabling the upper stage to return to Earth from orbit without thermal tiles. The nozzle accommodates deep throttle operation even in the presence of atmospheric pressure and serves as an actively cooled metallic heat shield during atmospheric reentry. There is also a center passive bleed that aims to create an aerospike engine-like effect for improved efficiency.

Specifications
  • Stages
    2
  • Length
    40.2 m
  • Diameter
    4.2 m
  • Fairing Diameter
  • Launch Mass
    227.0 T
  • Thrust
    3110.0 kN
Family
  • Name
    Nova
  • Family
  • Variant
  • Alias
  • Full Name
    Nova
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    3000.0 kg
  • Geostationary Transfer Orbit
    2500.0 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity

Stoke Space

Private
CEO: Andy Lapsa
Stoke 2020

Stoke Space Technologies is an American space launch company based in the Seattle suburb of Kent, Washington.

Upcoming Spaceflights


Nova | Demo Flight

Stoke Space | United States of America
Cape Canaveral SFS, FL, USA
TBD December, 2026
Status: To Be Determined
Mission:

First launch of Stoke Space’s Nova launch vehicle. Payload on board and planned reusability of the 2 stages is TBD.

Unknown
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