Piper AE- NE- HE- Cup
Entwicklung
Versionen
HE-1
AE-1
-
HE-1
AE-1
-
NE-1
-
NE-1
-
NE-2
-
NE-2
-
Einsatzgeschichte
The HE-1 was an ambulance
version of the Piper Cub and 100 were ordered. The rear fuselage
hinged up to permit
loading of a single patient on a stretcher. In 1943 the remaining HE-1s
were redesignated as AE-1.
A training version with dual controls, 230 were ordered as NE-1 and 20
as NE-2. In
February 1944 two NE-1s were used to test the use drone aircraft in
combination with M type airships to bomb submarines.
Bestellt
Zeichnungen
..
-
Technische Daten
| Specifications |
Piper L-4J |
|
|
Wingspan |
Spannweite |
10.76 m |
|
Length |
Länge |
6.88 m |
|
Height |
Höhe |
2.02 m |
|
Wing area |
Flügelfläche |
16.54 m2 |
|
Engine |
Motor |
Lycoming
0-290-D2 C flat four 125 hp |
|
Maximum speed |
Höchstgeschwindigkeit |
201 Km/h |
|
Empty weight |
Leergewicht |
474 Kg |
|
Loaded weight |
Startgewicht |
710 Kg |
|
Climb Rate |
Steigrate |
4.4 m/s |
|
Service ceiling |
Gipfelhöhe |
5'215 m |
|
Range |
Reichweite |
400 Km |
|
Armament |
Bewaffnung |
none |
| Capacity | Zuladung | 1 Pilot, 1 Passenger |
| Serial, Piper NE HE- Cup | ||
|
NE-1 |
26196 - 26425 |
230 |
|
NE2 |
29669 - 29688 |
20 |
|
NE2 |
29689 - 29698 |
(10) |
|
AE-1 |
30197 - 30296 |
100 |
|
Total |
350 |
|
