Saturn IB: Forskelle mellem versioner
Content deleted Content added
m Bot: fix datolink |
MGA73bot (diskussion | bidrag) m Retter udgået parameter til nyt |
||
Linje 6:
|oprindelse = [[USA]]
|cpl = 18 millioner [[USD]]<ref name="space launch report">{{cite web|title=Saturn IB History|work=Space Launch Report|author=Ed Kyle|url=
http://www.spacelaunchreport.com/satstg2.html|
|cpl-år = [[1965]]
|alt-cpl = 750 millioner [[DKK]] i [[2013]]
Linje 29:
|trinnr = Første
|navn = [[S-IB]] ([[Apollo 7]])
|længde = 24,44 m<ref name="Launch Vehicle Key Facts">{{cite web|http://history.nasa.gov/SP-4029/Apollo_18-11_Launch_Vehicle-Spacecraft_Key_Facts.htm|title=Apollo Launch Vehicle/Spacecraft Key Facts|
|diameter = 6,55 m
|tom = 38.342 kg<ref name="Ground Ignition Weights">{{cite web|url=http://history.nasa.gov/SP-4029/Apollo_18-19_Ground_Ignition_Weights.htm|title=Apollo Ground Ignition Weights|
|total = 450.831 kg
|motorer = 8× [[Pratt & Whitney|Rocketdyne]] [[H-1 (raketmotor)|H-1]]
|kraft = 7.759.477 [[Newton (enhed)|N]]
|SI = 272 s
|brændetid = 144,32 s<ref name="Apollo 7">{{cite web|url=http://history.nasa.gov/SP-4029/Apollo_07a_Summary.htm|title=APOLLO 7 - The First Mission: Testing the CSM in Earth Orbit|
|brændstof = [[Petroleum|RP-1]]/[[Ilt|LOX]]
}}
|