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Raptor, Cryogenic methane-fueled rocket engine

Discussion in 'SpaceX' started by HVM, Aug 9, 2016.

  1. HVM

    HVM Savolainen

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    #1 HVM, Aug 9, 2016
    Last edited: Aug 9, 2016
    WOW, SpaceX raptor program is advanced more, that I think before:

    C. G. Niederstrasser ‏@RocketScient1st

    "Shotwell - just shipped first Raptor engine to Texas last night. #SpaceX #smallsat"

    And Texas means here, the SpaceX Rocket Development and Test Facility in McGregor,

    Blah, Grendal ninjaposted me.
     
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  2. Grendal

    Grendal Active Member

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    Sorry about that.... :)
     
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  3. HVM

    HVM Savolainen

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    Raptor Specs:

    Cycle: Full-flow staged combustion
    Oxidizer: Subcooled liquid oxygen
    Fuel: Subcooled liquid methane
    Chamber Pressure: 300 bar
    Throttle Capability: 20% to 100% thrust

    Sea-Level Nozzle
    Expansion Ratio: 40
    Thrust (SL): 3,050 kN
    Isp (SL): 334 s

    Vacuum Nozzle
    Expansion Ratio: 200
    Thrust: 3,500 kN
    Isp: 382 s


    There should be two turbopumps and two pre-burners +turbines, can you find them?
    raptor.jpg
     
  4. siai47

    siai47 Member

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    I don't know anything about rocket engines---however a nice picture. Could the pumps be compound pumps? There appears to be one on the side and one of the top of the engine. The nozzle section looks more like the high bay lights in my shop---sure would be bright if lit up but would most likely clean out the shop before departing through the roof :) !
     
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  5. HVM

    HVM Savolainen

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    Nasaspaceflightcom's AP3 have same idea; guess for a flow diagram:
    Raptor_flow.jpg
    Where a LOX Pump, Turbine and the Preburners are integrated same blog as Combustion Chamber.
     
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  6. HVM

    HVM Savolainen

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    Interesting claim in NSF, about IPD and SpaceX.

    "The integrated powerhead demonstrator (IPD) was an U.S. Air Force project in the 1990s and early 2000s run by NASA and the Air Force Research Laboratory (AFRL) to develop a new rocket engine front-end (powerhead) that would utilize a full flow staged combustion cycle (FFSCC). The prime contractors were Rocketdyne and Aerojet.

    Future engine development work beyond the powerhead demo was never funded by the US government, and neither Rocketdyne—nor later Aerojet Rocketdyne after a 2013 merger—chose to pursue such development with their own or other private funding."
    -WIKI

    Apollo100 (NSF):
    "...Given that SX acquired the IPD Final report, all of the drawings, and all of the hardware, I would imagine that there is quite a bit of IPD heritage in the Raptor engine."
     
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  7. Grendal

    Grendal Active Member

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    Chris B - NSF on Twitter

    Chris B. wrote: Baby Raptor sure packs a punch! Photo by Gary Blair from an airplane over McGregor (well outside of any restricted area of course!).
    Here is the picture of the Raptor burn markings:

    Raptor.jpg
     
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