Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 References  





2 External links  














Hadley engine







Add links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


Hadley
Country of originUnited States
DesignerUrsa Major Technologies
StatusInitial Production
Liquid-fuel engine
PropellantLOX / Kerosene
CycleStaged 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

[edit]
  1. ^ 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
  • [edit]


  • t
  • e
  • t
  • e

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Hadley_engine&oldid=1212902257"

    Categories: 
    Rocket engines using kerosene propellant
    Rocket engines using the staged combustion cycle
    Outer space stubs
    Aircraft engine stubs
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    All stub articles
     



    This page was last edited on 10 March 2024, at 03:16 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki