PEGAS with Asparagus Staging about pegas HOT 2 CLOSED

First of all, my sincere apologies for a very late reply. I am currently very busy with other projects and, sadly, I admit I have neglected PEGAS. I will try to be more attentive of it in the future.

Regarding the actual issue. Although I haven't tried myself, it should already be possible to implement asparagus staging in PEGAS - the only nuance is that you have to do (some of) the math yourself. Let's assume there is one core booster and n secondary boosters that will be jettisoned in pairs. For simplicity we will assume that those boosters are exactly same as the core booster - both in mass and engines (it's still doable if they differ, although with more math to work through). Since it's asparagus, all of the boosters are fed from the last two ("last" meaning: those that will be jettisoned next) -- the strong assumption is that whenever you stage, you drop two empty tanks, and all of the remaining tanks are fully fueled (as if the rocket was brand-new).
Some symbols now:

• Mt -- total mass of the vehicle
• Mb -- total wet mass of each booster
• Mf -- mass of the fuel in each booster
• Fb -- thrust of a single booster

If we denote Mr as mass of the second stage (that is, rocket after the asparagus phase), then we can say that Mt = Mr + (n + 1) * Mb.

Defining the first stage is the crucial point in understanding this. Its total mass and engine setup will remain the same (as if you weren't doing asparagus) - the only difference will be in massFuel, since PEGAS calculates the staging time basing on this information. You want to drop the secondary boosters when they run out, so your massFuel is equal to 2 * Mf (this is saying: hit stage when all of the engines burn through the fuel contained in the last two boosters). Your engines have thrust of (n + 1) * Fb.

The next stage will now be a fully-fueled rocket, just without two of the boosters - . massTotal is the old Mt minus 2 * Mb and massFuel again is 2 * Mf - after all, you want to stage after depleting the two boosters which are now the last ones. Of course, you have to modify the total engine thrust by subtracting the contribution of the two dropped ones: thrust will be equal to (n - 1) * Fb (initial count minus 2).

For the final stage this is all slightly different. Since now you only have the core booster supporting the rest of the stack, your massTotal becomes Mr + Mb and massFuel is just Mf (only a single booster of fuel to burn). The thrust of your engines is also only Fb because you have the single core burning the fuel.

I hope this clears things up. For the less symmetric setup (i.e. your core booster has more/less engines than each of the jettisonable ones) you will probably have to use the full power of the engines system and define each booster as a separate engine, letting PEGAS do the thrust/mdot summation math. Possibly also the masses calculation will be a little different, but with this explanation I think you should be able to do this on your own.
In case of any further questions, please reply in this thread and I'll try to give you any help I can.

from pegas.

Thanks, I have found a really crude way of solving my problem by tricking the computer into thinking that the amount of fuel in the center stage is the amount gained from the outer boosters + the total fuel used in the center stage and it works fine. I will try and make a more refined version using actual algebra.

from pegas.