S.T.E.M: Space Mission Design V2

	B	C	D	E	G	H	I	J
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2	O	S.T.E.M. FOR THE CLASSROOM						O
3		Adventures in Outer Space
4		Space Mission Design App
5		Based on the Boeing Space Tug Study Design circa 1971
6		O					O
7		Periapsis Altitude	282	km	Mission Payload	8,900	kg
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9		Apoapsis Altitude	901	km	Average Selling Price	$1,500	/carat
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11		On-Station Time	14	days	Lunar Investment	$27.14	B (USD)
12		O					O
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14		O		O	O		O
15		Periapsis Delta V	179	mps	Transfer Time	0.03	days
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17		Apoapsis Delta V	175	mps	Round Trip Time	0.06	days
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19		Delta V + Reserve	356	mps	Mission Duration	14.06	days
20		O		O	O		O
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22		O		O	O		O
23		CM Static	1,489	kg	Lunar Material	8,220	kg
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25		CM Dynamic	2,814	kg	Gross Income	$61.65	B (USD)
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27		CM Weight	4,303	kg	Taxable Income	$34.51	B (USD)
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29		Crew Size	11	people	Return On Investment	127.14	%
30		O		O	O		O
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32		O		O	O		O
33		Orbiter Gross Weight	17,040	kg	Lander Gross Weight	40,340	kg
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35		Orbiter Propellant	1,292	kg	Lander Propellant	24,186	kg
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37		Excess Propellant	16,761	kg	Excess Propellant	-6,133	kg
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39		Orbiter LH2	189	kg	Lander LH2	3,531	kg
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41		Orbiter LO2	1,104	kg	Lander LO2	20,655	kg
42		O		O	O		O
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44	O	Copyright © 2017 S.T.E.M. for the Classroom. All rights reserved. Patent Pending.						O
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