March 2000 | 5100 | 0057-2317-MTDC |
Greg Lovellette, Project Leader
The Aircraft Use Triangle addresses cost effectiveness, use of the correct aircraft, and safety. While cost effectiveness and use of the correct aircraft are important parameters in choosing the drop height for an airtanker, safety must be the most important factor.
Low-altitude retardant drops from fixed-wing airtankers may injure firefighters. Injuries are caused by flying debris (such as treetops or rocks) or when firefighters are knocked down. If the retardant has lost all of its forward momentum and is falling vertically as a heavy rain, the danger to firefighters is minimal. Safe drop height can be defined as the distance below the airtanker at which the retardant begins to fall vertically. Figure 1 shows a drop that was released from a safe drop height, has lost all forward motion, and is falling vertically. Figure 2 shows a drop that was released below the safe drop height and still had considerable forward motion when it reached the ground.
Figure 1— Retardant drop released
from a safe height.
Figure 2—Retardant drop intentionally
released
below
the safe drop
height during testing.
Video and films of drop tests for a variety of airtankers dropping full and partial loads have been examined. The distance below the aircraft where retardant began to fall vertically was recorded and compared to the flight and release characteristics. From these data, a relationship between safe drop height, peak flow rate, and load size was developed. The relationship can be expressed as:
S = 101 + 0.0112 * L + 0.0202 * P + 50
Where S = Safe drop height in feet
L = Load size in gallons
P = Peak flow rate in gallons per second.
The additional 50 feet are a safety factor. The formula does not accurately represent constant-flow tanks and single-engine airtankers. The data table uses actual measurements for these airtankers.
Table 1 lists each type of fixed-wing airtanker approved by the Interagency Airtanker Board and the safe drop height for full and partial loads. The safe drop height for trail drops depends on the interval between releases. To determine the safe drop height for trail drops treat the total volume being released as if it were a single release.
Airtankers are listed by the manufacturer of the tank and gating system rather than by the operator of the airtanker. Airtanker numbers are shown to help determine the type of tank on each airtanker.
Safe drop height (feet above impact) | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
Airtanker type |
Airtanker numbers |
Tank volume |
Flow setting |
Full Load |
1/2 Load |
1/3 Load |
1/4 Load |
1/6 Load |
1/8 Load |
1/16 Load |
ARDCO Aero Flite DC-4 ARDCO Aero Flite DC-4 |
65, 119, 151, 152, 160,161, 166 65, 119, 151, 152, 160,161, 166 |
2000 2000 |
High Low |
319 231 |
192 170 |
192 170 |
172 161 |
|||
Aero Union Corp. C-130 Aero Union Corp. C-130 Aero Union Corp. C-130 Aero Union Corp. C-130 Aero Union Corp. C-130 Aero Union Corp. C-130 Aero Union Corp. C-130 Aero Union Corp. C-130 |
30, 31, 63, 64, 67 30, 31, 63, 64, 67 30, 31, 63, 64, 67 30, 31, 63, 64, 67 30, 31, 63, 64, 67 30, 31, 63, 64, 67 30, 31, 63, 64, 67 30, 31, 63, 64, 67 |
3000 3000 3000 3000 3000 3000 3000 3000 |
1/2 1 2 3 4 6 8 9 |
130 137 145 150 169 185 190 249 |
130 137 145 150 169 185 190 |
130 137 145 150 169 185 |
130 137 145 |
|||
Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion Aero Union Corp. P3 Orion |
00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 00, 22, 23, 25, 26, 27, 21 |
3000 3000 3000 3000 3000 3000 3000 3000 |
1/2 1 2 3 4 6 8 Max |
140 149 166 175 204 223 253 310 |
140 149 166 173 200 215 242 244 |
140 149 166 173 194 204 196 |
140 149 166 166 192 |
|||
Aero Union Corp. SP2H Aero Union Corp. SP2H Aero Union Corp. SP2H Aero Union Corp. SP2H Aero Union Corp. SP2H Aero Union Corp. SP2H Aero Union Corp. SP2H |
01, 03, 16, 18 01, 03, 16, 18 01, 03, 16, 18 01, 03, 16, 18 01, 03, 16, 18 01, 03, 16, 18 01, 03, 16, 18 01, 03, 16, 18 |
2000 2000 2000 2000 2000 2000 2000 2000 |
1/2 1 2 3 4 5 6 ED |
128 135 143 156 169 196 215 234 |
128 135 143 150 169 173 173 173 |
128 135 143 150 |
128 135 143 |
|||
Aero Union Conventional C-54 - DC-4 Aero Union Conventional C-54 - DC-4 |
14, 15 14, 15 |
2000 2000 |
High Low |
260 202 |
207 180 |
180 171 |
169 161 |
|||
Aero Union Conventional DC-7 Aero Union Conventional DC-7 |
33, 60, 62, 66 33, 60, 62, 66 |
3000 3000 |
High Low |
284 219 |
221 188 |
189 171 |
170 163 |
|||
Hawkins & Powers C-130 Hawkins & Powers C-130 |
81, 83, 88, 130, 131, 133 81, 83, 88, 130, 131, 133 |
3000 3000 |
High Low |
287 241 |
219 196 |
185 173 |
168 163 |
|||
Hawkins & Powers KC-97 Hawkins & Powers KC-97 Hawkins & Powers KC-97 |
97 97 97 |
3200 3200 4000 4000 |
High Low High Low |
323 290 348 298 |
237 219 257 228 |
196 186 204 190 |
174 169 178 171 |
162 160 164 160 |
||
Hawkins & Powers SPB4Y2 Hawkins & Powers SPB4Y2 Hawkins & Powers SPB4Y2 Hawkins & Powers SPB4Y2 |
121, 123, 124, 126, 127 121, 123, 124, 126, 127 121, 123, 124, 126, 127 121, 123, 124, 126, 127 |
2200 2200 2000 2000 |
High Low High Low |
265 235 254 223 |
208 193 203 187 |
180 172 177 169 |
165 162 164 160 |
|||
Marsh Turbo Thrush 60/40 Door Marsh Turbo Thrush 60/40 Door Marsh Turbo Thrush 60/40 Door |
380 380 380 |
40% Door 60% Door Both Doors |
80 90 100 |
|||||||
Minden Air Inc. P2V-7 Minden Air Inc. P2V-7 Minden Air Inc. P2V-7 Minden Air Inc. P2V-7 |
55, 99 55, 99 55, 99 55, 99 |
2450 2450 2000 2000 |
High Low High Low |
288 231 283 228 |
221 170 217 162 |
199 145 196 139 |
176 123 175 121 |
|||
Neptune, Inc. P2V-7 H & P P2V-7 Neptune, Inc. P2V-7 H & P P2V-7 |
08, 09, 10, 11, 139, 140 08, 09, 10, 11, 139, 140 |
2450 2450 |
High Low |
288 215 |
219 183 |
199 172 |
175 162 |
|||
Neptune Inc. P2V-5 Neptune Inc. P2V-5 |
05, 06, 07 05, 06, 07 |
2450 2450 |
High Low |
291 214 |
221 182 |
201 173 |
178 163 |
|||
Pierce Turbo Thrush | 450 | 80 | ||||||||
Snow Airtractor 802 Snow Airtractor 802 Snow Airtractor 802 Snow Airtractor 802 Snow Airtractor 802 Snow Airtractor 802 |
181, 182 181, 182 181, 182 181, 182 181, 182 181, 182 |
800 800 800 800 800 800 |
1/2 1 2 3 4 Max |
92 102 123 151 179 186 |
92 102 123 151 179 186 |
92 102 116 151 144 144 |
||||
Western Pilot Services Dromader – Melex gate |
500 | 140 | ||||||||
Western Pilot Services Dromader – Transland |
500 | 100 |
Greg Lovellette is a Physical Scientist at MTDC. He received a Bachelor of Science degree in Chemistry at the University of Montana in 1980. Before joining the Forest Service in 1989, he worked as an oil well analyst throughout Montana, Wyoming, and North Dakota.
Additional single copies of this
document may be ordered from:
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Development Center
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Missoula, MT 59808-9361
Phone: (406) 329-3978
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E-mail: wo_mtdc_pubs@fs.fed.us
For additional technical
information, contact Greg
Lovellette at the address above.
Phone: (406) 329-4815
Fax: (406) 329-3719
Lotus Notes: Greg Lovellette/WO/USDAFS
E-mail: glovellette@fs.fed.us
An electronic copy of this
document is available on the
Forest Service’s FSWeb Intranet
at:
http://fsweb.mtdc.wo.fs.fed.us
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