The following values are required for computing the ballistics analysis:

• Mass \(m\) in kg
• Caliber/Diameter \(d\) in m
• Thrust force per given engine stage \(F_E\) in N
• Drag coefficient \(C_d\)
• Rho liquid consonant \(p\) as determined by the altitude formula
• Velocity \(V\) in m/s
• altitude \(D_h\) in m

Value \(p\) is estimated by following approximation

\( 3.0099 - 0.868106 \log_{e}(0.0014659D_h + 7.88959) \)

The formula is only accurate from 0 to 10000 barometric meters of altitude

Drag for any given velocity is determined by this formula

\( F_D\ = C_d * \frac{ p * V^{2} }{2} * d * \pi \)

The final distance per flight section achieved \( \Delta d \) is determined through the sum of integrals for each engine-phase.

The constraints \(a\) and \(b\) represent the phase of flight in seconds, where \( x = V \) and \( a > t(F_E) > b \).

Each flight section \(a\) to \(b\) is determined by the total engine stages + 1 (terminal phase where \( F_E = 0 \)).

\( \Delta d = \int_a^b \,dx = \frac{F_E - F_D}{m} \)

The entire implementation of the formulas can be found here.

Name	Description	Unit	better: ▲higher ▼lower
Name	Name used for internal files	-	-
Range	Simulated range the missile will reach determined by the formulas above	m	▲
MaxSpeed	Hard limit for the missiles velocity	m/s	▲
DeltaV	Theoretical maximum acceleration excluding air resistance	m/s²	▲
LaunchG	Maximum G load the carrier aircraft may experience at launch	g = 9.81m/s²	▲
FlightG	Mid-flight peak G load the missile may accelerate with	g = 9.81m/s²	▲
Rear aspect	Distance the missiles IR seeker can track an aircraft exhaust	m	▲
All aspect	Distance the missiles IR seeker can track an aircraft signature	m	▲
IR decoys	Visible distance to infrared countermeasures such as flares	m	▼
IRCM	The visible distance to IRCM	m	▼
FOV	FOV from the main seeker	deg	▼
Gate	Field of view the seeker gains after lock	deg	▼
LaunchFov	Maximum distance from the bore to the seekers gimbal before launch	deg	▲
FlightFov	Maximum distance from the bore to the seekers gimbal after launch	deg	▲
WarmUpTime	Time required to ready the seeker	s	▼
WorkTime	Time the seeker is active	s	▲
Time out	Time the seeker is inactive after launch	s	▼
Uncage	Weather or not the seeker can gimbal off bore before launch	bool	▲
Radar slave	Permits radar slaving of the missile	bool	▲