def main(argv):
"""Determine basic vehicle propellant and mass parameters of vehicle."""
parsed = parseargs(argv)
#writer = HTML(sys.stdout)
writer = Text(sys.stdout)
putrow = writer.putfmtrow
putitem = writer.putitem
basicrept = BasicLV(writer)
fh = open(parsed.vehicle, 'r')
design = yaml.load(fh)
fh = open(parsed.propellants, 'r')
propeldb = yaml.load(fh)
if parsed.verbose:
import pprint
pp = pprint.PrettyPrinter(width=41, stream=sys.stderr)
pp.pprint(["design", design])
performance = multistage.performance(design)
sequence = design['stageorder']
deltaVlist = []
putitem('Mass and deltaV:')
for activestage in sequence:
putitem('Stage: ' + activestage)
stageperf = performance[activestage]
basicrept.putStageMassesDeltaV(activestage, stageperf)
deltaVlist.append(stageperf['deltaV'])
totalDeltaV = sum(deltaVlist)
putitem('Total deltaV:')
putrow('Total deltaV (m/s, ft/s)', '%11.4f', [totalDeltaV, totalDeltaV*m2ft])
reptfmts = {}
reptfmts['propel.deduce'] = propel.reptfmt_deduce
stages = design['stages']
for activestage in sequence:
stageperf = performance[activestage]
if 'Isp' not in stages[activestage] or stages[activestage]['Isp'] == 0:
continue
mixture = stages[activestage]['mixture']
Mpropel = stageperf['Mignite']-stageperf['Mburnout']
propellants = propel.deduce(propeldb, mixture, Mpropel)
stageperf['gRange'] = design['gRange']
flows, reptflows = propel.flows(propellants, stageperf)
reptfmts['propel.flows'] = reptflows
basicrept.putPropellants(activestage, stageperf, propellants, reptfmts)
putitem('Totals:')
drytot = multistage.masses(design['stageorder'], stages, mtype='Mdry')
putrow('dry mass', '%11.4f', [drytot, drytot/lb2kg])
def main(argv):
"""Determine basic vehicle propellant and mass parameters of vehicle."""
parsed = parseargs(argv)
writer = Text(sys.stdout)
putrow = writer.putfmtrow
putitem = writer.putitem
putrow("msglabel", "%8s", [ "hello", "world" ])
fh = open(parsed.vehicle, 'r')
design = yaml.load(fh)
fh = open(parsed.propellants, 'r')
propeldb = yaml.load(fh)
staging = multistage.performance(design)
sequence = design['stageorder']
maxG = design['maxG']
for activestage in sequence:
stageinfo = staging[activestage]
putitem ('%-32s Mignite %7.1f Mburnout %7.1f kilo' % (activestage,
stageinfo['Mignite'], stageinfo['Mburnout'] ))
putitem ('%-32s Mignite %7.1f Mburnout %7.1f lbm' % (activestage,
stageinfo['Mignite']/lb2kg, stageinfo['Mburnout']/lb2kg ))
putitem ('%-32s deltaV %7.1f' % (activestage, stageinfo['deltaV']))
deltaV = staging['totalDeltaV']
putrow ('Total deltaV (m/s, ft/s)', '%11.4f', [deltaV, deltaV*m2ft])
stages = design['stages']
for activestage in sequence:
stageinfo = staging[activestage]
if 'Isp' not in stages[activestage] or stages[activestage]['Isp'] == 0:
continue
mixture = stages[activestage]['mixture']
Mpropel = stageinfo['Mignite']-stageinfo['Mburnout']
propresults = propel.deduce(propeldb, mixture, Mpropel)
putitem ('Stage: ' + activestage)
for label, fmt, prop in (
('matl names', '%7s', 'matlNames'),
('liqdens (kg/l)', '%7.3f', 'liqdens'),
('masses (kg)', '%7.3f', 'masses'),
('volume (l)', '%7.3f', 'volumes') ):
results = list(propresults[prop])
if prop == 'matlNames':
results.append('[sum]')
elif prop in ('masses', 'volumes'):
results.append(sum(propresults[prop]))
putrow (label, fmt, results)
avgdens = sum(propresults['masses'])/sum(propresults['volumes'])
putrow ('avg dens (kg/l)', '%11.4f', [avgdens])
# compute thrust based on stageinfo['Mburnout']
thrust = stageinfo['Mburnout'] * gEarth * maxG
wIgnite = stageinfo['Mignite'] * gEarth
wBurnout = stageinfo['Mburnout'] * gEarth
deltaV = stageinfo['deltaV']
mflow = thrust / (stageinfo['Isp'] * gEarth)
wetmass = stageinfo['Mignite']
drymass = stageinfo['Mburnout']
burntime = Mpropel / mflow
GIgnite = thrust / wIgnite
GBurnout = thrust / wBurnout
for label, fmt, values in (
('massflow (kg/s)', '%11.4f', [mflow]),
('burn time (s)', '%11.4f', [burntime]),
('G (ignite, burnout)', '%7.3f', [GIgnite, GBurnout]),
('thrust (N, lbf)', '%11.4f', [thrust, thrust*N2lb]),
('wt ignite (N, lbm)', '%11.4f', [wIgnite, wIgnite*N2lb]),
('wt burnout (N, lbm)', '%11.4f', [wBurnout, wBurnout*N2lb]),
('deltaV (m/s, ft/s)', '%11.4f', [deltaV, deltaV*m2ft]),
('wet mass', '%11.4f', [wetmass, wetmass/lb2kg]),
('dry mass', '%11.4f', [drymass, drymass/lb2kg]), ):
putrow (label, fmt, values)
putitem ('Totals:')
drytot = multistage.masses(design['stageorder'], stages, mtype='Mdry')
putrow ('dry mass', '%11.4f', [drytot, drytot/lb2kg])
