Originally posted by Nate
What the heck is going on here?!?
This is the third informative thread I've read on here this morning! we're actually getting into some legitimate discussions finally! woot!
Catocene- with a name like that I certainly don't doubt your expertise, but I have a hard time seeing how adding a chemical to your motor can increase ISP. NH4ClO4 is an amazingly powerful oxidizer, and anytime you remove a percentage of AP to replace it with a different metal (oxidizer or not) you're going to subtract from the overall performance of the motor.
Please, correct me if I'm wrong....
You're wrong. (How's that for service?)
But seriously, you're mostly right, with one minor caveat: oxidizer content is not the only important variable. It's by far the most important one, but there are others.
If you look through any of the standard reference texts (Sutton's _Rocket Propulsion Elements_, for example), you'll find that quite a bit of (largely government-sponsored) research has gone into optimizing APCP performance in terms of maximizing Isp.
For propellant using common polybutadiene (HTPB or PBAN) binders, you actually get the highest Isp by including a small amount of metal powder -- typically Aluminum, magnesium, or magnalium (an Al/Mg alloy) -- in addition to the AP and binder/fuel. I don't have it in front of me, but I seem to remember the optimum ratio being somewhere around 70/17/13 for AP/Al/PBAN. I'll look it up at lunch (my copy of Sutton is out in my truck).
The metal powder increases the flame temperature, opacifies the propellant, and also serves as a fuel, itself. Higher flame temperature usually means more complete combustion *inside* the motor, which means less fuel is wasted *outside* the motor. Also, higher temps mean higher kinetic energy of the gas molecules, which translates directly to more thrust.
To ensure that combustion takes place only at the surface of the grain, the grain needs to be opaque to the infrared radiation due to the combustion. A mixture of *just* AP and PBAN or HTPB is translucent; usually an opacifier such as lampblack must be added to prevent catos from the whole grain trying to ignite all at once. Metal powder replaces the low-molecular weight lampblack carbon with a denser Al or Mg, improving volumetric loading (basically a measure of overall density, including the empty space in the motor core), and giving a more-reactive fuel with a higher flame temperature.
It's also possible to substitute even-more-reactive ingredients for some of the AP to get even slightly-higher performance propellants. However, this is typically only done for specific military purposes, as the ingredients in question tend to be extremely hazardous, either in terms of stability, toxicity, or both. Most are high-order explosives, like nitroglycerine, RDX, etc.
For amateur and commercial rocketry purposes, AP is just about the best possible solid oxidizer, and the various rubber binder chemicals like PBAN and HTPB have excellent physical and chemical properties for propellant use. APCP with AP/Al/Binder gives just about the highest performance you can get without significant compromises in other areas.
(Of course, so-called "knob" motors, which are designed for effects like colored flames and sparks, rather than pure performance, are another kettle of fish entirely....)
- Rick "Flame on" Dickinson