|
Data Comparison
Comparing the onboard RDAS
flight computer downloaded
the next day, with the data
seen in real-time from the
rocket in flight, we can see
very close reporting between
all the sensors flown on
this test flight:
|
Standard GPS time to
apogee |
00:25.00 |
|
HP
GPS time to apogee
(GPS) |
00:20.00 |
|
HP
GPS time to apogee (Baro) |
00:18.25 |
|
Rdas
time to apogee |
00:17.70
|
|
|
|
|
Max
Standard GPS |
4,759.51
Realtime |
|
Max
HP GPS |
4,538.39
Realtime |
|
Max
Baro |
4,627.09
Realtime |
|
Max
RDAS |
4,698.00
Download |
|
|
|
|
RDAS
Delta from Each
Unit: |
|
|
Standard GPS |
61.51 |
|
HP
GPS |
(159.61) |
|
HP
GPS Baro |
(70.91) |
As shown above, the
real-time data download
coming from the rocket in
flight was extremely
accurate. Recovery was
made .38 miles away in deep
sage. |

 |
|
As shown here, the
rocket's electronics bay
contained two STXe units
wrapped in bubble-wrap to
help offset the G-forces.
Neither STXe was mounted to
the airframe, but both were
snug inside the avionics
bay.
The STXe units were both
still sending data from the
ground once the unit hand
landed.
|

|