Differences between revisions 36 and 38 (spanning 2 versions)

Propellant Plume Gas Scattering

Estimated hydrogen mass per 1000 km height, 1.67e-27kg/H
Altitude km	1000	2000	10000	20000	30000	35786*	40000	50000	60000	69572*	70000
Radius km	7378	11378	16378	26378	36378	42164*	46378	56378	66378	75950*	76378
Volume km³	6.8e11	1.6e12	3.4e12	8.7e12	1.7e13	2.2e13	2.7e13	4.0e13	5.5e13	7.2e13	7.3e13
#H / m³	2.1e10	1.2e10	8.2e8	1.8e8	6.7e7	4.5e7	2.2e7	3.5e7	1.4e7	1.1e7	1.0e7
H kg	24000	32000	18000	12000	5100	2500*	2300	2300	1300	1300*	1200

Less than 20 tonnes of hydrogen (and almost nothing else) above GEO, out to the bow shock.

The second column is the combined collision cross section with an H₂ molecule ... the square of the sum of the square roots.

-  ⇤ ← Revision 36 as of 2019-09-19 06:21:40 → 
  Size: 2535
  Editor: KeithLofstrom
  Comment:
+   ← Revision 38 as of 2020-08-27 06:36:38 → ⇥
  Size: 2535
  Editor: KeithLofstrom
  Comment:
-Deletions are marked like this.
+Additions are marked like this.
 Line 29:
-|| #H /  m³    || 2.1e10 || 1.2e10 || 3.1e9  || 8.2e8  || 1.8e8  || 6.7e7  || 4.5e7  || 3.5e7  || 1.4e7  || 1.1e7  || 1.0e7  ||
+|| #H /  m³    || 2.1e10 || 1.2e10 || 8.2e8  || 1.8e8  || 6.7e7  || 4.5e7  || 2.2e7  || 3.5e7  || 1.4e7  || 1.1e7  || 1.0e7  ||

Diff for "GasScatter"