Predictions based on missile geometry

[husker]

Hi all,

I would like to start a discussion about what features can be predicted of a missile based on its known outer geometry. There are a few things thatI can list as follows:

Lift coefficient
Drag coefficient
A suitable engine fits in the geometry
Average thrust
Cruise speed
etc.

What are your opinions?
How would you investigate that geometry in terms of design and tactical aspects?

Best Regards

 

[husker]

Moreover,

Maximum altitude
Cruise altitude
Maneuverability
Static/Dynamic stabilty
Radar Cross Section

And, your suggestions?

 

[Just Some Guy]

you forgot this:
- cost
- IR signature
- interoperability
- warhead size/type
and
- cost

 

[husker]

Thank you. You are correct.

I think these can be added to the list:

Required air volume for the engine
Average hydraulic dimater of the air intake (depends on the altitude)
Average fuel consumption of the engine
Maximum flight time (Within an interval)
Maximum range (Within an interval)
Maximum eeight (Within an interval)

By the way, I accept that some of these estimations have greater margins.

What can else be added?

Regards