03-11-2010, 07:14 AM
[quote name='Arun_S' date='10 March 2010 - 03:46 PM' timestamp='1268257118' post='105055']
I guess I should specify the stage configuration when I report Agni-V's satellite capability. This one is for this confign.
[/quote]
Except for thrust directions and launch direction, this config file is the same as the one on pg 7 of this thread. So much altitude difference ? Also, payload in this file is the same as that of last file. So, you must say 750kg - ~200kg for guidance and navigation syatems, etc. So, is'nt orbital payload ~550 kg rather than 700 kg ?
I guess I should specify the stage configuration when I report Agni-V's satellite capability. This one is for this confign.
Code:
Payload = 750.0 Kg, Number of Stages = 4, Simulation Time Granularity = 0.100 Second
Launch Direction = 110 degrees-North, Launch Latitude = 22.00 degrees
Segment-Name ISP(Vac) ISP(SL) Stage-Mass Fuel-Fract Burn-Time Thrust-Direction Diameter Length ThrustOverdrive OverdrivePeriod
Stage1 269.0 237.0, 33,000.0 0.900 080.0 Sec 50.0 Degree 2.00 Meter 07.00 Meter 15.00 % 20.00 %
Stage2 290.0 190.0, 14,000.0 0.870 060.0 Sec 25.0 Degree 2.00 Meter 03.50 Meter 10.00 % 10.00 %
PayloadAdaptor 000.0 000.0, 00,150.0 0.700 001.0 Sec 00.0 Degree 2.00 Meter 03.30 Meter 00.00 % 00.00 %
Stage3 290.0 200.0, 03,500.0 0.850 030.0 Sec 10.0 Degree 2.00 Meter 02.00 Meter 00.00 % 00.00 %[/quote]
Except for thrust directions and launch direction, this config file is the same as the one on pg 7 of this thread. So much altitude difference ? Also, payload in this file is the same as that of last file. So, you must say 750kg - ~200kg for guidance and navigation syatems, etc. So, is'nt orbital payload ~550 kg rather than 700 kg ?