Space Programs and Technologies Conference 1990
DOI: 10.2514/6.1990-3794
|View full text |Cite
|
Sign up to set email alerts
|

Mission profiles for human Mars missions

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

1992
1992
2015
2015

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 8 publications
(1 citation statement)
references
References 0 publications
0
1
0
Order By: Relevance
“…T = m6 =u.rh (57) where mi6 is force of thrust, rh is the change of the rocket mass due to propellant loss and u, is the velocity of the exhaust gas (27:8-15) (47:2).…”
Section: Mars Transfer Vehiclementioning
confidence: 99%
“…T = m6 =u.rh (57) where mi6 is force of thrust, rh is the change of the rocket mass due to propellant loss and u, is the velocity of the exhaust gas (27:8-15) (47:2).…”
Section: Mars Transfer Vehiclementioning
confidence: 99%