Talk:SpaceX reusable launch system development program/Archive 1: Difference between revisions
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*'''km/h''' and '''mph''' conversions, assuming 90,000 feet altitude for Mach 6 and 120,000 feet altitude for Mach 10, which approximates the launch profile for this [[RP1]]/[[LOX]] first-stage booster.
**<code><nowiki>{{convert/q|6|Mach|90000|abbr=on}}</nowiki></code> yields: <nowiki>{{convert/q|6|Mach|90000|abbr=on}}</nowiki>
**<code><nowiki>{{convert/q|10|Mach|120000|abbr=on}}</nowiki></code> yields: <nowiki>{{convert/q|10|Mach|120000|abbr=on}}</nowiki>
*'''km/s''' conversions, assuming 90,000 feet altitude for Mach 6 and 120,000 feet altitude for Mach 10, which approximates the launch profile for these [[RP1]]/[[LOX]] first-stage boosters.
**<code><nowiki>{{convert/q|6|Mach|km/s|mph|90000|sigfig=2|disp=flip|sp=us|abbr=on}}
</nowiki></code> yields: <nowiki>{{convert/q|6|Mach|km/s|mph|90000|sigfig=2|disp=flip|sp=us|abbr=on}}</nowiki>
**<code><nowiki>{{convert/q|10|Mach|km/s|mph|120000|sigfig=2|disp=flip|sp=us|abbr=on}}
</nowiki></code> yields: <nowiki>{{convert/q|10|Mach|km/s|mph|120000|sigfig=2|disp=flip|sp=us|abbr=on}}</nowiki></small>
===Proposal for handling the Mach no. sources===
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