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Kestrel (rocket engine)

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Title: Kestrel (rocket engine)  
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Subject: SpaceX, Falcon 1, SpaceX rocket engine family, Draco (rocket engine family), Merlin (rocket engine family)
Collection: Rocket Engines, Rocket Engines Using Kerosene Propellant, Spaceflight, Spacex Rocket Engines
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Kestrel (rocket engine)

Kestrel 2
SpaceX Kestrel
Country of origin United States
First flight 2006
Last flight 2009
Designer Tom Mueller
Manufacturer SpaceX
Application upper stage boost
Liquid-fuel engine
Propellant LOX / RP-1
Cycle pressure fed
Performance
Thrust (vac.) 6,900 pounds-force (31 kN)
Thrust-to-weight ratio 65
Chamber pressure 135 pounds per square inch (930 kPa)
Isp (vac.) 317 seconds (3.11 km/s)
Dimensions
Dry weight 52 kilograms (115 lb)
References
References [1][2][3]
Kestrel engine test firing.

The Kestrel engine is an LOX/RP-1 pressure-fed rocket engine. The Kestrel engine was developed by SpaceX for upper stage use on the Falcon 1 rocket.

Kestrel was built around the same pintle architecture as the Space X Merlin engine but does not have a turbo-pump and is fed only by tank pressure.

Kestrel is ablatively cooled in the chamber and throat and radiatively cooled in the nozzle, which is fabricated from a high strength niobium alloy. As a metal, niobium is highly resistant to cracking compared to carbon-carbon. According to SpaceX, an impact from orbital debris or during stage separation might dent the metal but have no meaningful effect on engine performance.[4] Helium pressurant efficiency is substantially increased via a titanium heat exchanger on the ablative/niobium boundary.[5]

Thrust vector control is provided by electro-mechanical actuators on the engine dome for pitch and yaw. Roll control (and attitude control during coast phases) is provided by helium cold gas thrusters.

A TEA-TEB pyrophoric system is used to provide multiple restart capability on the upper stage. In a multi-manifested mission, this allows for drop off at different altitudes and inclinations.

Kestrel 2

Enhancements to the design of the original Kestrel engine were planned, called the Kestrel 2.[6]

The engine was planned to continue to be pressure-fed design, but was to have flown on a newly designed second stage that was to use Aluminium-lithium alloy 2195 rather than the 2014 Aluminum used in the Falcon 1 second stage.[6] Engine changes were to include tighter tolerances to improve consistency, higher Isp, and lighter weight.[7] The Kestrel 2 did not remain in active development after the Falcon 1 was replaced by the much larger Falcon 9 v1.0 which used an improved Merlin 1C for its upperstage.

See also

References

  1. ^ "Falcon 1 Users Guide" (PDF). SpaceX. 2008-09-28. 
  2. ^ spachelaunchreport.com - falcon
  3. ^ astronautix
  4. ^ Greg Zsidisin (23 March 2007). "SpaceX Confirms Stage Bump On Demoflight 2". Space Daily. Retrieved 2008-09-30. 
  5. ^ "Falcon 1 Flight Three Press Kit" (PDF). SpaceX. Retrieved 2008-09-30. 
  6. ^ a b Bjelde, Brian; Max Vozoff; Gwynne Shotwell (August 2007). "The Falcon 1 Launch Vehicle: Demonstration Flights, Status, Manifest, and Upgrade Path". 21st Annual AIAA/USU Conference on Small Satellites (SSC07 ‐ III ‐ 6). Retrieved 2013-12-06. 
  7. ^ Bergin, Chris; Braddock Gaskill (2007-09-24). "Elon Musk Q and A - Updates SpaceX status on Falcon and Dragon". NASAspaceflight.com. Archived from the original on 2008-05-29. Retrieved 2008-06-16. 

External links

  • SpaceX Falcon engines page
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