News on the SpaceX propulsion front. Not official so exact numbers may change after the tests, but very close. This speedup is possible because of a hiring spurt - they're between 1,400 and 1,500 souls now and still growing. Seems resume's from engineers are staked up like cord wood, but they're picky.
1) Merlin 2 is a go and under active development. It will have a thrust of about 1,000,000 lb-ft (4,448,500 Newtons) - similar to the Rocketdyne RS-84 (which they have the rights to) and about 2.5x the thrust of the Space Shuttle Main Engine (!). Quite likely it'll be lighter, cheaper to build and simpler than either of those. Very possible it'll be an advanced staged combustion engine.
2) the Raptor liquid hydrogen/LOX second stage is also in active development. No details on it yet other than it'll be a staged combustion engine, but it would be used for high energy destinations like geostationary orbits, Mars, heavier lunar or asteroid missions..
3) a new variant of Falcon 9 is in the works that will replace the Merlin 1C engine cluster and MVac 2nd stage engine with the Merlin 2 and the Raptor. Very likely it'll also get higher capacity tanks up and down. A beast.
4) the Merlin 1C Block II engine is getting replaced with the Merlin 1D, which is now undergoing tests at their McGregor, Texas test site. Word is it's exceeding its goals.
This is a huge upgrade in that its weight has been reduced 33%, its part count drastically reduced (ex: down to a single servo from 13) and the whole thing made into a production line engine. All this and a major performance update too (see below)
The throttleability means that Falcon 9 will no longer have to shut down 2 of its 9 engines at maximum dynamic pressure (Max-Q), but simply ease up on the gas. This will also mean a very, very smooth ride for astronauts in the Dragon.
5) a new MVac 2nd stage engine is also in the works based on the new Merlin 1D for use in the Falcon Heavy
6) if a Merlin 2 version of Falcon Heavy would be built or if they'll go straight to a larger diameter core like Falcon X or Falcon XX is an open question.
1) Merlin 2 is a go and under active development. It will have a thrust of about 1,000,000 lb-ft (4,448,500 Newtons) - similar to the Rocketdyne RS-84 (which they have the rights to) and about 2.5x the thrust of the Space Shuttle Main Engine (!). Quite likely it'll be lighter, cheaper to build and simpler than either of those. Very possible it'll be an advanced staged combustion engine.
2) the Raptor liquid hydrogen/LOX second stage is also in active development. No details on it yet other than it'll be a staged combustion engine, but it would be used for high energy destinations like geostationary orbits, Mars, heavier lunar or asteroid missions..
3) a new variant of Falcon 9 is in the works that will replace the Merlin 1C engine cluster and MVac 2nd stage engine with the Merlin 2 and the Raptor. Very likely it'll also get higher capacity tanks up and down. A beast.
4) the Merlin 1C Block II engine is getting replaced with the Merlin 1D, which is now undergoing tests at their McGregor, Texas test site. Word is it's exceeding its goals.
This is a huge upgrade in that its weight has been reduced 33%, its part count drastically reduced (ex: down to a single servo from 13) and the whole thing made into a production line engine. All this and a major performance update too (see below)
The throttleability means that Falcon 9 will no longer have to shut down 2 of its 9 engines at maximum dynamic pressure (Max-Q), but simply ease up on the gas. This will also mean a very, very smooth ride for astronauts in the Dragon.
5) a new MVac 2nd stage engine is also in the works based on the new Merlin 1D for use in the Falcon Heavy
6) if a Merlin 2 version of Falcon Heavy would be built or if they'll go straight to a larger diameter core like Falcon X or Falcon XX is an open question.
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