In-flight break-up involving Airbus Zephyr unmanned aerial Vehicle Wyndham, WA 28/09/18:
Details:
Following test flights in the northern hemisphere, the Zephyr 8 was positioned to Wyndham, WA for further research and development. Powered by batteries and solar, this 25m wingspan UAV operates in the Stratosphere (up to 74000ft (this is above the Troposphere, which contains all of Earth’s weather)). While the Zephyr had previously completed a 25-day flight, the ultimate goal was to achieve a flight of over 100 days.
As the Zephyr was susceptible to turbulence on its 10-hour climb through the Tropopause, the mission had been abandoned on the previous day due to unsuitable surface winds. Other unsuitable weather for the Zephyr’s climb was identified as layers of air which included both rising and descending air (mixing layer) of greater depth than 1500ft. This was found to be less likely at night.
On the evening of 28 September 2019, the Zephyr was launched at 9:43pm in what was considered, ‘ideal’ conditions. At 1200ft, an uneventful systems check was conducted. The UAV continued to climb in a South Easterly direction. With a climb rate of 5000ft per hour, at 10:40pm it passed 5200ft and experienced an uncommanded roll of 15 degrees to the right, changing track by approximately 180 degrees.
As this was believed to be due to thermal turbulence from a dry salt lake, a northerly track towards smoother air was selected. However, at 11:07pm, passing 8700ft , the UAV again experienced an uncommanded roll of 14 degrees to the right, followed by an uncommanded roll of 17 degrees to the left. Again, the aircraft self corrected however the conditions persisted resulting in a 1000ft descent over 7 mins.
The crew increased power and tried to maneuvre the aircraft to an area they believed had smoother air, however at 1115pm it experienced another uncommanded right roll, from which it was slow to recover. During the recovery it exceeded its maximum airspeed, then with full left rudder applied, the roll angle increased beyond limits and entered an uncontrolled spiral dive. At 11:16pm the airspeed increased beyond Vne and both wings fractured around mid span resulting in an inflight break-up.
Using FDODAR, let’s analyse the accident:
Think about each of the stages: What do the students think happened within the FDODAR model?
What other options could this crew have discussed? (Refer to the “Options” slide):
Were this team too Mission focused in their decisions? (From the “Decision” slide):