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The Wikipedia article for the Common Booster Core says is uses Liquid O2 and Liquid H2. Where is Hydrazine used in the process?
Hydrazine is not Hydrogen, and Hydrogen is not (effectively) storable. It shure is nasty stuff, though, I agree with that! The Draco series uses Monomethyl Hydrazine and N2O4 as the hypergolic components.Sure does. Hydrazine is nasty stuff though.
Hydrazine - Wikipedia, the free encyclopedia
SpaceX will use hydrogen/hydrazine in the SuperDraco and Draco engines.
SuperDraco - Wikipedia, the free encyclopedia
You are correct. My error. Hydrazine is used in the Centaur upper stage which is often used by ULA.
This is not surprising given that SpaceX has a Falcon Heavy animation that shows 3 cores landing.SpaceX is having an environmental assessment done to build two more landing pads at the Cape for multiple FH booster and center core landings.
SpaceX is having an environmental assessment done to build two more landing pads at the Cape for multiple FH booster and center core landings.
Nope not surprising at all but good to know. I'm actually a little surprised F9 will return to flight this year.
I don't see a link to that announcement in your post or @Grendal post just above yours. Would like to read your source. Thanks!Nope not surprising at all but good to know. I'm actually a little surprised F9 will return to flight this year.
I don't see a link to that announcement in your post or @Grendal post just above yours. Would like to read your source. Thanks!
In talk on COSMIC-2, NOAA says Falcon Heavy demo launch scheduled for 2nd Q
It looks like SpaceX is focusing on March, April, or May for the Falcon Heavy launch. I'm guessing a bit but I expect that SpaceX was holding out for the F9 design to be fully vetted. Now we know that there is still one major upgrade still to come. You have wonder how powerful FH will be when it eventually uses 3 Block 5 cores.... That version should be as powerful as the proposed New Glenn from Blue Origins and SLS Block 1.
Jeff Foust on Twitter
SpaceX was also looking into the possibility of refueling the cores on the landing platform and having them fly back to land under their own engine power.