ChartObject Chart 1

 plot P/(S+T)


nuclear steamer solar steamer LOX/LH2 solar LH2 LH2 arcjet
         
pstdeltaV pstdeltaV pstdeltaV pstdeltaV pstdeltaV
3000 3950 3950 3950 3950
m/s m/s m/s m/s m/s
         
pstpower pstpower pstpower pstpower pstpower
3000 0.01 1300 0.01 0.001
megawatts megawatts megawatts megawatts megawatts
         
time time time time time
0.5 100 0.0125 100 100
days days days days days
         
pstship pstship pstship pstship pstship
100 0.05 1 0.05 0.05
tons tons tons tons tons
         
ullage ullage ullage ullage ullage
0.1 0.1 3 3 0.1
percent percent percent percent percent
         
tankage tankage tankage tankage tankage
0.01 0.1 10 10 0.1
percent tank per fuel masses percent tank per fuel masses percent tank per fuel masses percent tank per fuel masses percent tank per fuel masses
         
         
         
pstPsp pstPsp pstPsp pstPsp pstPsp
1296000000 1728000000 1404000000 1728000000 172800000
j/kg j/kg j/kg j/kg j/kg
         
         
         
         
         

 
 
 
ChartObject Chart 1

 
 
 
 
 
ChartObject Specific Power or Propellant Massfor 20 tons to Lunar Escape

 
 
 
 
 
ChartObject Power/Mass  vs Specific Impulse

 
 
 
 
 
 
ChartObject Specific Power and Mass Ratio vs Mass Delivered Per Engine

 
 
 
 
 
 
ChartObject Specific Power vs tons engine per ton deliveredto Low Lunar Orbit

 
 
 
 
 
 



Last Updated on 3/22/98
By anthony