From Wikipedia, the free encyclopedia
Hadley
Country of originUnited States
Designer Ursa Major Technologies
StatusInitial Production
Liquid-fuel engine
Propellant LOX / Kerosene
Cycle Staged combustion
Performance
Thrust, sea-level5,000 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

  1. ^ a b "Ursa Major Technologies wants outsourcing engines to be the norm". SpaceNews. 2018-09-09. Retrieved 2022-03-24.
  2. ^ 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.
  3. ^ "Stratolaunch Celebrates First Powered Flight of TA-1 Test Vehicle".
  4. ^ "Ursa Major Hadley Engine Flies for the First Time" (Press release).
  5. ^ "ABL Space Systems increases performance and cuts price of its small launch vehicle". SpaceNews. 2019-02-01. Retrieved 2022-03-24.
  6. ^ Launch System 2: Upper Stage Engine, retrieved 2023-04-24

External links


From Wikipedia, the free encyclopedia
Hadley
Country of originUnited States
Designer Ursa Major Technologies
StatusInitial Production
Liquid-fuel engine
Propellant LOX / Kerosene
Cycle Staged combustion
Performance
Thrust, sea-level5,000 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

  1. ^ a b "Ursa Major Technologies wants outsourcing engines to be the norm". SpaceNews. 2018-09-09. Retrieved 2022-03-24.
  2. ^ 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.
  3. ^ "Stratolaunch Celebrates First Powered Flight of TA-1 Test Vehicle".
  4. ^ "Ursa Major Hadley Engine Flies for the First Time" (Press release).
  5. ^ "ABL Space Systems increases performance and cuts price of its small launch vehicle". SpaceNews. 2019-02-01. Retrieved 2022-03-24.
  6. ^ Launch System 2: Upper Stage Engine, retrieved 2023-04-24

External links



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