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« SB 600 | Main | CALIFORNIA DTSC SEEKING TO AMEND UPA REGS »

October 30, 2005

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ルイヴィトン スーパーコピー

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ルイヴィトン スーパーコピー

Audeilla

Sadly, none of the Russian boosters have a prtaiculraly good Isp; the Apollo-derived SSME has a very high chamber pressure, and as such an exceptionally high exhaust velocity.Remember that a rocket can't accelerate a payload past the thermal velocity of its exhaust gases; for the SSME, that's about 14km/sec. Ariane 5 s core engine could do it, too; it almost does (the solids are only really there to punch through the soupy sea-level atmosphere )

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