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S A Weather Service Aero Commanders

 

The South African Weather Service is equipped with 2 twin prop, pressurized Aero Commander 690 A’s. These aircraft have been used in weather modification experiments and also atmospheric chemistry studies. The design of the Aero Commanders lends to use in harsh environments, like severe icing and turbulence, warm temperatures, high altitudes and long endurance. This makes them ideal for use in atmospheric research.

The specifications of these aircraft are given in table a. The instruments used on the aircraft are given in tables b,c,d and e. The aircraft are capable of carrying 6 particle probes. One of the aircraft has a high quality window for photography and radiometry. On board data acquisition enables in flight decision-making. The aircraft is also flexible and can be modified to carry almost any type of instrument.

Figure 1 shows a picture of ZS-JRA and figure 2 shows ZS-JRB.

a) Aero Commander Technical Information
Aircraft length: 44'4.25''
Aircraft wingspan: 46'6.64''
Aircraft height: 14'11.35''
Maximum gross weight: 10 250 lbs
Nominal operating altitude: 25 000' to 28 000' AMSL
Maximum operating altitude: 31 000' AMSL
Minimum speed: 82 KTS
Nominal cruise speed: 245 KTS
Maximum speed: 260 KTS @ 25000' (as equipped)
Nominal sampling speed: 100 to 180 KTS
Nominal rate of climb: 1200'/min@ 18000' & 120KTS & 10000lbs
Maximum rate of climb: 3400'/min@ 2000'MSL & 140KTS & 9000lbs
Endurance with maximum fuel: 5.5 HRS @ 5000'MSL & 150KTS (no reserve)
Crew Capacity: 1 to 4 (with instrument racks)
Cabin payload at maximum gross weight: 1880lbs @ MAX ZERO FUEL WEIGHT
Cabin dimension: 110.24'' x 47.24''
Entrance door dimension: 47'' x 26.5''
Interior cabin passage way dimension: 9.843'' BETWEEN SEATS
Standard equipment rack dimension: 43.31'' x 19.69'' x 15.748''
Floor mounting track width 13.1583''
Electrical power: 28 VDC; 12 kW
2kW@ 220VAC, 60Hz
1kW@ 115VAC, 60Hz
4kW@ 115VAC, 400Hz

b) Navigation and Flight Characteristics
Parameter Technique Manufacturer Range*(resolution)
Latitude and longitude Global positioning system Trimble TNL2000 global
Position tracks Telemetry ESD 120km
Ground speed Global positioning system Trimble TNL2000 global
True speed Derived from Pitot and Static pressure Rosemount 10 to 300 KTS
Pitch, role and heading Synchro to digital ESD 0 to 359 degrees (0.08 degrees RES)
Angle of Attack Variable resistance transducer Rosemount +‑23 degrees
Altitude Derived from Static pressure Rosemount 0 to 30000 ft

c) General Meteorological
Parameter Technique Manufacturer & Model Range*(resolution)
Total air temperature Platinum wire resistance Rosemount Model 102AU1AF -50 to +50 degrees Celsius
Static air temperature Reverse‑flow thermometer Inhouse 30 to +50 degrees Celsius
Humidity Reverse‑flow humidity sensor Inhouse 0 to 100%
Static Pressure Pressure Transducer Rosemount Model 1201FA1B2B 0 to 32 Hg
Pitot Pressure Pressure Transducer Rosemount Model 1201FA1B2B 0 to 5 psi

d) Cloud Physics
Parameter Technique Manufacturer & Model Range*(resolution)
Liquid water content Hot wire resistance Johnson & Williams 0 to 2 and 0 to 6 g.m**‑3
Liquid water content Hot wire resistance King / PMS 0 to 5 g.m**‑3
Liquid water content Particle measurement FSSP100 / PMS 0 to 5 g.m**‑3
Size spectrum of cloud particles Forward light scattering FSSP100 / PMS 2 to 47 microns (15 channels)*
Images of cloud particles Diode occultation imaging OAP2D C / PMS 25 to 800 micron Resolution 25 micron*
Images of precipitation particles Diode imaging OAP2DP / PMS Resolution 200 micron*

e) Data acquisition cards
Card type Function and Resolution Quantity Manufacturer
Timer and Keypad Sample rate and hot keys 1card ESD
Analog to Digital 16 channels, 16 bit, Bipolar (+‑10V) 2 cards ESD
Synchro to Digital 3 channels, 16 bit 2 cards ESD
PMS 1D 15 channels & activity & Total Strobes 2 cards ESD
PMS 2D Image Acquisition 2 cards ESD
Serial 232/422 Port GPS interface 1 ESD

*all particle sizes refer to maximum particle dimension

Figure 1. ZS-JRA in flight
Figure 1. ZS-JRA in flight

Figure 2. ZS-JRB in flight
Figure 2. ZS-JRB in flight


 
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