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) --------------------------------------------------------------------------
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