Impressive numbers out of that Raptor V3 test. Chamber pressure 350 bars vs 200 for SSME.
More generally, seems they want a pretty high T/W for SH-Starship: 1.5 to 1.7. The objective: cut into the gravity losses by shooting off the pad ASAP.
For the record: while the ISS circle the world at an orbital velocity of 7800 m/s, ascending to it must include steering, drag, and gravity losses. While steering is small and drag not too large, gravity losses are the real bastard: pushing the tally by way more than 1000 m/s: way beyond 9000 m/s.
Delta 7925 with its many GEM solids seemingly managed to cut into its gravity losses enough, to sneak below 9000 m/s to orbit. So it can be done. Wonder if SH-Starship could manage the same feat with a lot of Raptor thrust right off the pad (provided the pad doesn't become a smoldering hole in the ground, but that's another matter !).
More generally, seems they want a pretty high T/W for SH-Starship: 1.5 to 1.7. The objective: cut into the gravity losses by shooting off the pad ASAP.
For the record: while the ISS circle the world at an orbital velocity of 7800 m/s, ascending to it must include steering, drag, and gravity losses. While steering is small and drag not too large, gravity losses are the real bastard: pushing the tally by way more than 1000 m/s: way beyond 9000 m/s.
Delta 7925 with its many GEM solids seemingly managed to cut into its gravity losses enough, to sneak below 9000 m/s to orbit. So it can be done. Wonder if SH-Starship could manage the same feat with a lot of Raptor thrust right off the pad (provided the pad doesn't become a smoldering hole in the ground, but that's another matter !).