markp
Active member
Well I'm getting some of the specs from the DRM1 document. The rest is guesswork.
Quoting the DRM1 document:
And this is figure 3-16:

I am then using wikipedia to find the thrust of a F1A :
http://en.wikipedia.org/wiki/Rocketdyne_F-1
Then I am working backwards to find the mass of the propellant for the rocket assuming the empty mass of the rocket is 1000 tons, which might be a bit high.
So far I have the following numbers in the code. I'm still in the process of massaging the numbers so it has a sensible and efficient ascent profile.
masses
double empty_hlv = 1000000.0;
double fuel_hlv = 25108216.0;
double fuel_boosters = 0.5*fuel_hlv;
double fuel_1ststage = 0.4*fuel_hlv;
double fuel_2ndstage = 0.1*fuel_hlv;
thrust
double thrust_launch = 256121600; // 12 x F1A engines
Quoting the DRM1 document:
Option 4 (Figure 3-16) is indicative of a launch vehicle that uses technology derived from the Saturn V launch vehicle. The first stage core is virtually identical to the first stage of the Saturn V launch vehicle in its basic size and its use of five F-1A engines. Strapped to this stage are four boosters, each with two F-1A engines and roughly one-third of the propellant carried by the core stage. The second stage uses six of the J-2 engines that powered the second stage of the Saturn V. However, this upper stage is considerably larger than the Saturn second stage.
And this is figure 3-16:

I am then using wikipedia to find the thrust of a F1A :
http://en.wikipedia.org/wiki/Rocketdyne_F-1
Then I am working backwards to find the mass of the propellant for the rocket assuming the empty mass of the rocket is 1000 tons, which might be a bit high.
So far I have the following numbers in the code. I'm still in the process of massaging the numbers so it has a sensible and efficient ascent profile.
masses
double empty_hlv = 1000000.0;
double fuel_hlv = 25108216.0;
double fuel_boosters = 0.5*fuel_hlv;
double fuel_1ststage = 0.4*fuel_hlv;
double fuel_2ndstage = 0.1*fuel_hlv;
thrust
double thrust_launch = 256121600; // 12 x F1A engines
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