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celestlab >> Trajectory and maneuvers > CL_man_thrustDuration

CL_man_thrustDuration

Thrust duration as function of mass consumed

Calling Sequence

output = CL_man_thrustDuration(type_output, par1, par2, par3 [[, g0]])
dt = CL_man_thrustDuration('dt', dm, F, isp [[, g0]])
dm = CL_man_thrustDuration('dm', dt, F, isp [[, g0]])
F = CL_man_thrustDuration('F', dt, dm, isp [[, g0]])
isp = CL_man_thrustDuration('isp', dt, dm, F [[, g0]])

Description

Parameters

type_output:

String defining the parameter to be computed. It can be 'dt,'dm','F' or 'isp'. (1x1)

par1:

First input parameter: dt, dm, F or isp [s kg N or s] (PxN)

par2:

Second input parameter: dm, F or isp [kg N or s] (PxN)

par3:

Third input parameter: F or isp [N or s] (PxN)

g0:

(optional) value of gravity acceleration. [m/s^2] (default value is %CL_g0) (1x1)

output:

Value of computed parameter: dt, dm, F or isp [s kg N or s] (PxN)

Authors

Bibliography

See also

Examples

// mass consumed in kg
isp = 220; // seconds
dv = 1; // m/s
m = 180; // kg
dm = CL_man_consumption('dm',dv,m,isp);

// thrust duration in seconds
F = 1 ; // N
[dt] = CL_man_thrustDuration('dt',dm,F,isp)

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