Differences between revisions 1 and 15 (spanning 14 versions)

Interplanetary Launch

The launch loop is intended for launch velocities below escape, and vehicles of 5 tonnes or less. Interplanetary expeditions will require far more velocity and far larger vehicles. Large interplanetary vehicles will be assembled in orbit from many - perhaps thousands - of 5 tonne components, and fueled for escape (and eventual arrival) with hundreds of additional deliveries of propellant.

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Mean Free Path Versus Altitude
Altitude	Temp erature	Mean Free Path	. .	Altitude	Temp erature	Mean Free Path	. .	Altitude	Temp erature	Mean Free Path
km	Kelvin	km		km	K	km		km	K	km
75	208.4	9.8E-7		180	790.1	0.12		500	999.2	77
80	198.6	4.4E-6		200	854.6	0.24		550	999.7	150
90	186.9	2.4E-5		250	941.3	0.89		600	999.9	280
100	195.1	1.4E-4		300	976.0	2.6		700	1000	730
120	360.0	3.3E-3		350	990.1	6.7		800	1000	1400
140	559.6	1.8E-2		400	995.8	16		900	1000	2100
160	626.3	5.3E-2		450	998.2	36		1000	1000	3100

-  ⇤ ← Revision 1 as of 2020-11-10 01:53:04 → 
  Size: 1598
  Editor: KeithLofstrom
  Comment:
+   ← Revision 15 as of 2020-11-10 02:00:52 → ⇥
  Size: 1676
  Editor: KeithLofstrom
  Comment:
-Deletions are marked like this.
+Additions are marked like this.
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-||<9> Mean Free Path Versus Altitude                                                                 ||
|| Altitude || Temperature || Mean Free Path || Alt   || Temp  || M.F.P. || Alt   || Temp  || M.F.P. ||
|| km       || Kelvin      || km             || km    || K     || km     || km    || K     || km     ||
|| 75       || 208.4       || 9.8E-7         || 180   || 790.1 || 0.12   || 500   || 999.2 || 77     || 
|| 80       || 198.6       || 4.4E-6         || 200   || 854.6 || 0.24   || 550      || 999.7       || 150            ||  
|| 90       || 186.9       || 2.4E-5         || 250   || 941.3 || 0.89   || 600      || 999.9       || 280            ||
|| 100      || 195.1       || 1.4E-4         || 300   || 976.0 || 2.6    || 700      || 1000        || 730            ||
|| 120      || 360.0       || 3.3E-3         || 350   || 990.1 || 6.7    || 800      || 1000        || 1400           || 
|| 140      || 559.6       || 1.8E-2         || 400   || 995.8 || 16     || 900      || 1000        || 2100           ||
|| 160      || 626.3       || 5.3E-2         || 450   || 998.2 || 36     || 1000     || 1000        || 3100           |||
+||<-11> '''Mean Free Path Versus Altitude'''                                                            ||
|| Altitude || Temp<<BR>>erature || Mean<<BR>>Free<<BR>>Path || . . ||Altitude || Temp<<BR>>erature || Mean<<BR>>Free<<BR>>Path || . . || Altitude || Temp<<BR>>erature || Mean<<BR>>Free<<BR>>Path ||
|| km       || Kelvin      || km             || || km  || K     || km     || || km   || K     || km     ||
|| 75       || 208.4       || 9.8E-7         || || 180 || 790.1 || 0.12   || || 500  || 999.2 || 77     ||
|| 80       || 198.6       || 4.4E-6         || || 200 || 854.6 || 0.24   || || 550  || 999.7 || 150    ||
|| 90       || 186.9       || 2.4E-5         || || 250 || 941.3 || 0.89   || || 600  || 999.9 || 280            ||
|| 100      || 195.1       || 1.4E-4         || || 300 || 976.0 || 2.6    || || 700  || 1000        || 730            ||
|| 120      || 360.0       || 3.3E-3         || || 350 || 990.1 || 6.7    || || 800  || 1000        || 1400           ||
|| 140      || 559.6       || 1.8E-2         || || 400 || 995.8 || 16     || || 900  || 1000        || 2100           ||
|| 160      || 626.3       || 5.3E-2         || || 450 || 998.2 || 36     || || 1000 || 1000        || 3100           ||

Diff for "InterplanetaryLaunch"

Interplanetary Launch