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Raptor Engine - General Development Discussion and News

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Wonder if Elon’s tweet about them extending Super Heavy an extra 2 meters means they are getting higher performance than expected out of the Raptor.
Or maybe after switching Startship from carbon fiber to stainless steel Elon realized that the new design was so much heavier than before that extra propellant would be needed to get it to orbit.
 
Without context both are plausible, with the latter more likely. One could imagine better-than-expected performance being realized as the ability to stuff more payload mass in starship rather than stuffing more propellant on the sub orbital stage.

A few other plausible drivers could be:
—re-entry stability
—some weird harmonic
—more volumetric configurations at the top or the bottom (for perhaps additional thermal mitigation, plumbing, ease of manufacturing/refurbishment, better/easier starship integration)
 
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Not specifically Raptor but interesting:
104150923_10159887745662119_3177966428189320600_o.jpg
 
Differences are minor because this is a test engine; practically just same raptor with bigger nozzle, example flexible joint is still there. Vacuum-Merlin and sea level- one are almost different engines; same can be true with raptor too, when vac. version evolves.

Tweets:

Elon:

Worth noting that thrust is only slightly higher with the big bell nozzle version. Larger bell is primarily for efficiency in vacuum. Aiming for 380+ sec Isp for RVac long-term. Initially likely to be ~372.

@PPathole:
Elon, are those hinges required for thrust vectoring at the very top? Will those be used for mounting on the test stand?

Elon:
This is a test engine. Flight articles are fixed with no gimbal.

@Erdayastronaut:
Odds of it surviving its first test? Pretty confident it'll work perfectly or is the first run of a new nozzle design pretty risky with a low chance of success?

Elon:
Above 50% likely to make it

https://twitter.com/elonmusk/status/1302069036621033472
 
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