Hadley engine
| Country of origin | United States |
|---|---|
| Designer | Ursa Major Technologies |
| Status | Initial Production |
| Liquid-fuel engine | |
| Propellant | LOX / Kerosene |
| Cycle | Staged combustion |
| Performance | |
| Thrust, sea-level | 5,000 lbf (22 kN) |
The Ursa Major Technologies Hadley is a 22-kilonewton (5,000 lbf) thrust Kerosene/LOX oxidizer-rich staged combustion cycle rocket engine.
Hadley is the first engine developed by Ursa Major Technologies. It started development in 2015, and prototypes were test fired in 2018.[1] In March 2022 qualification of the engine was complete and flight-ready engines had been delivered to customers.[2] In March 2024 Stratolaunch Systems announced completion of the first powered flight of the Talon-A test vehicle, TA-1.[3] Hadley is the engine powering Talon-A.[4]
Another initial customer, Phantom Space Corporation, plans to use Hadley on their Daytona small-lift rocket.[2] ABL Space Systems initially announced they would use the Hadley engine for the upper-stage[1] of their RS1 rocket, but have subsequently decided to use an internally-developed engine called E2.[5] In April 2023, Astra suggested the vacuum variant of the Hadley engine would power the second stage of their Rocket 4.0 launch vehicle.[6]
References[edit]
- ^ a b "Ursa Major Technologies wants outsourcing engines to be the norm". SpaceNews. 2018-09-09. Retrieved 2022-03-24.
- ^ a b Berger, Eric (2022-03-23). "Ursa Major says its Hadley engine supports vertical launch and hypersonic uses". Ars Technica. Retrieved 2022-03-24.
- ^ "Stratolaunch Celebrates First Powered Flight of TA-1 Test Vehicle".
- ^ "Ursa Major Hadley Engine Flies for the First Time" (Press release).
- ^ "ABL Space Systems increases performance and cuts price of its small launch vehicle". SpaceNews. 2019-02-01. Retrieved 2022-03-24.
- ^ Launch System 2: Upper Stage Engine, retrieved 2023-04-24
External links[edit]
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