7 photos from Wikimedia Commons · credits & licences
- 1. Air Zoo December 2019 094 (Piasecki HUP-3 Retriever): Michael Barera· CC BY-SA 4.0
- 2. Piasecki XHJP-1 Retriever at Naval Air Station Patuxent River, circa in 1950 (NH 101806-KN): Commander Richard Timm, U.S. Navy· Public domain
- 3. Piasecki HUP Retriever delivers man to USS Boston (CAG-1), in 1957 (L45-33.02.05): Wikimedia Commons· Public domain
- 4. Piasecki HUP-2 Retriever (Bu128533) (50341630492): tormentor4555· PDM-owner
- 5. Piasecki HUP-2 Retriever hovers over USS Boston (CAG-1), circa in 1959: U.S. Navy· Public domain
- 6. Piasecki HUP-2 Retriever of HU-1 lands aboard USS Worcester (CL-144), in 1957: U.S. Navy· Public domain
- 7. Piasecki HUP-2 Retriever of HU-2 aboard USS Pittsburgh (CA-72) in the Mediterranean Sea, 1954 (2021.14): Wikimedia Commons· Public domain
what is it?
The Piasecki HUP Retriever or H-25 Army Mule, later UH-25, is a compact single radial engine, twin overlapping tandem rotor utility helicopter developed by the Piasecki Helicopter Corporation of Morton, Pennsylvania. Designed to a United States Navy specification, the helicopter was produced from 1949 to 1954, and was also used by the United States Army and foreign navies. The HUP/H-25 was the first helicopter to be produced with an autopilot and also the first to perform a loop.
How to recognise it: 1 piston engine · 10.7 m main rotor
base stats
Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).
fun facts
- First flew 78 years ago, in 1948.
- Rotor of 10.7 m: about 2 cars parked nose to tail.
piston: A car-like piston engine turning a propeller: simple and cheap, the classic small plane.
spec sheet
- first flight
- 1948-03
- introduced
- 1949
- retired
- 1964
- status
- retired
- number built
- 339
- role
- utility helicopter
- makers
- Piasecki Helicopter Corporation
- engines
- 1× Continental R-975-46A
- length
- 17.4 m
- rotor diameter
- 10.7 m
- height
- 4 m
- max take-off weight
- 2,767 kg
- top speed
- 169 km/h
- cruise speed
- 129 km/h
- range
- —
- ceiling
- 3,048 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q3382217, Wikipedia: Piasecki HUP Retriever (CC BY-SA 4.0).Updated 2026-10-24.