SpaceX Kestrel

From WikiProjectMed
(Redirected from Kestrel (rocket engine))
Jump to navigation Jump to search
SpaceX Kestrel
SpaceX Kestrel
Country of originUnited States
First flight2006
Last flight2009
DesignerTom Mueller
ManufacturerSpaceX
ApplicationUpper stage boost
Liquid-fuel engine
PropellantLOX / RP-1
CyclePressure fed
Performance
Thrust, vacuum28 kN (2.9 tf)
Thrust-to-weight ratio65
Chamber pressure9.3 bar (135 psi)
Specific impulse, vacuum317 seconds (3.11 km/s)
Dimensions
Dry weight52 kg (115 lb)
References
References[1][2][3]
Kestrel engine test firing.

The SpaceX Kestrel was an LOX/RP-1 pressure-fed rocket engine. The Kestrel engine was developed in the 2000s by SpaceX for upper stage use on the Falcon 1 rocket. Kestrel is no longer being manufactured; the last flight of Falcon 1 was in 2009.

Kestrel was built around the same pintle architecture as the SpaceX Merlin engine but does not have a turbopump and is fed only by tank pressure.

Kestrel was ablatively cooled in the chamber and throat and radiatively cooled in the nozzle, which was 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 ignition system is used to provide multiple restart capability on the upper stage. In a multi-manifested mission, this design would allow 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 design was still pressure-fed, and was supposed to fly on a newly designed second stage that used 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 upper stage.

See also

References

  1. ^ "Falcon 1 Users Guide" (PDF). SpaceX. 2008-09-28. Archived from the original (PDF) on October 1, 2008.
  2. ^ spachelaunchreport.com - falcon
  3. ^ astronautix Archived 2013-12-16 at the Wayback Machine
  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. Archived from the original (PDF) on 2008-10-01. 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

Wikimedia Commons has media related to Kestrel (rocket engine).
Retrieved from "https://mdwiki.org/wiki/SpaceX_Kestrel"