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timelines:us_launch_rockets [2016/03/13 15:10] – [Saturn IC] michel vantimelines:us_launch_rockets [2019/03/29 15:13] (current) – external edit 127.0.0.1
Line 2: Line 2:
  
 ====Saturn V==== ====Saturn V====
 +
 +America heavy lift rocket build for Apollo program.
  
 SA-500F Facilities integration test model  SA-500F Facilities integration test model 
Line 39: Line 41:
 ====Saturn VB====  ====Saturn VB==== 
 consisting of an standard S-IC and S-IIB (with five J-2S) and S-IVC (one J-2S) consisting of an standard S-IC and S-IIB (with five J-2S) and S-IVC (one J-2S)
-new J-2S engine (S for Simplified) which led to a reduction of Stage mass, higher ISP and options for restarting the upper stage several time+new J-2S engine (S for Simplified) which led to a reduction of Stage mass, higher ISP and options for restarting the upper stage several time, the Payload is increased by 9%
  
 SA-600  modified SA-500D for new engine  SA-600  modified SA-500D for new engine 
Line 118: Line 120:
 SA-303 standby Spacelab Rescue Mission(not used) SA-303 standby Spacelab Rescue Mission(not used)
  
-SA-304 with Centaur third stage to bring German HELIOS to Sun +SA-304 with Centaur third stage to bring German HELIOS to Sun orbit
  
-SA-305 Spacelab 5 Mission +SA-305 with Centaur third stage to bring Viking 1 to Mars 
  
-SA-306 +SA-306 with Centaur third stage to bring Viking 2 to Mars 
  
-SA-307 +SA-307 Spacelab 5 Mission. 
  
 SA-308  SA-308 
timelines/us_launch_rockets.1457896235.txt.gz · Last modified: 2019/03/29 15:19 (external edit)

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