Welcome to Deployability Engineering! TEA logo

Air Transportability (Revised)

(Applique)

   

C-130

       

HIMARS

33,500

278 X 96 X 106

1

1

4

5

 

XM1120 LHS (empty)

35,500

422 X 96 X 106

1

1

3

5

 

XM1120 (partial load)

59,300

422 X 96 X 129

0

0

2

3

C-17, 2 at 65,000

XM1120 (GVW)

66,000

422 X 96 X 129

0

0

1

2

C-5, 3 at 59,000

MTVR (empty)

   

1

2

4

6

 

MTVR (cross-country)

38,200

 

1

1

3

4

 

MTVR (highway)

44,500

 

0

1

2

4

 

.

CONCEPT AND ANALYSIS EQUIPMENT

NOTE: Characteristics subject to change. May not reflect potential dimensional reductions for aircraft loading.

NOTE: The U.S. Army is NOT acquiring the LAV-III, but is instead acquiring an Interim Armored Vehicle (IAV) based on the LAV-III concept. The LAV-III is currently in production for the Canadian Army and is included as a concept vehicle only. The IAV has a C-130 transport requirement. We will update this page with IAV data when it becomes available.

 

Weight
(pounds)

L x W X H
(inches)

C-130

C-141

C-17

C-5

Notes

AGLS L-1

37,000

365 X 100 X 106

1

1

3

4

 

AGS L-3

52,000

365 X 130 X 120

0

0

2

3

 

FLYER

7,000

179 X 80 X 60

2

5

10

14

 

 

 

Old URL: http://www.tea.army.mil/dpe/Aircraft%20loads.htm

Webpage has been removed

Page 7 of 8