[amsat-bb] H-IIA F26 launch procedure

[Masahiro Arai]

Here is the launch procedure for H-IIA F26 rocket which is launcher of
Sinen2 and ARTSAT2.


H-IIA F26 launch time:  04:24:48z  30th Nov, 2014
Main payload:  Hayabusa2 -- Asteroid Explorer
Piggyback payloads:  Sinen2, ARTSAT2-DESPATCH, PROCYON


                event                    T      altitude  inertial velocity
                                      HH:MM:SS     km           km/s
---------------------------------------------------------------------------
 1  liftoff                           00:00:00        0          0.4
 2  solid rocket booster burnout      00:01:39       46          1.6
 3  solid rocket booster separation   00:01:48       53          1.6
 4  fairing separtion                 00:04:10      137          2.8
 5  1st stage main engine cuttoff     00:06:36      202          5.6
 6  1st/2nd stage separation          00:06:44      207          5.6
 7  2nd stage engine ignition#1       00:11:18      254          7.8
 8  2nd stage engine cuttoff#1        00:11:18      254          7.8
 9  2nd stage engine ignition#2       01:39:23      250          7.8
10  2nd stage engine cuttoff#2        01:43:24      313         11.8
11  Hayabusa2 separation              01:47:15      889         11.4
12  Sinen2 separation                 01:53:55     2867         10.4
13  ARTSAT2-DESPATCH separation       01:58:05     4418          9.7
14  PROCYON separation                02:02:15     6068          9.2


Separation location(lat/lon) for Sinen2 is around 0/190, ARTSAT2 is
around -6/199.


73

Masa    JN1GKZ