DVAKM:

Path: Orbit/OrbitManeuver

% Computes the temperature required to achieve the desired delta-V.

   Since version 1.
--------------------------------------------------------------------------
   Form:
   [tReq, dV3Sig, iTReq] = DVAKM( iT, temp, threeSig, mF, mO, dV )
--------------------------------------------------------------------------

   ------
   Inputs
   ------

   iT          (1,2)  Total impulses (Ns)
   temp        (1,2)  Corresponding temperatures
   threeSig           Three sigma variation in impulse
   mF                 Fuel mass (kg)
   m0                 Initial mass (including fuel) (kg)
   dV                 Desired delta-V (m/sec)

   -------
   Outputs
   -------
   tReq               AKM Temperature
   dV3Sig             Three sigma delta-V (m/sec)
   iTReq              Required impulse (N-s)

--------------------------------------------------------------------------

Back to the Orbit Module page