S.T.E.M. for the Classroom: Space Mission Design

	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		kg
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9		Apoapsis Altitude	101,003	km	Average Selling Price		/carat
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11		On-Station Time	18	days	Lunar Investment		B (USD)
12		O					O
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14		O		O	O		O
15		Periapsis Delta V	3,025	mps	Transfer Time	0.75	days
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17		Apoapsis Delta V	1,332	mps	Round Trip Time	1.49	days
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19		Delta V + Reserve	4,389	mps	Mission Duration	19.49	days
20		O		O	O		O
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22		O		O	O		O
23		CM Static	1,489	kg	Lunar Material		kg
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25		CM Dynamic	2,828	kg	Gross Income		B (USD)
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27		CM Weight	4,317	kg	Taxable Income		B (USD)
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29		Crew Size	10	people	Return On Investment		%
30		O		O	O		O
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32		O		O	O		O
33		Orbiter Gross Weight		kg	Lander Gross Weight		kg
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35		Orbiter Propellant		kg	Lander Propellant		kg
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37		Excess Propellant		kg	Excess Propellant		kg
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39		Orbiter LH2		kg	Lander LH2		kg
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41		Orbiter LO2		kg	Lander LO2		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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