3 photos from Wikimedia Commons · credits & licences
- 1. Hiller Hornet, c. 1949, helicopter powered by ramjet propulsion on rotor tips - Hiller Aviation Museum - San Carlos, California - DSC03033: Daderot· CC0
- 2. Hiller XHOE-1 Hornet - DPLA - cd5d7372b219be9958abee336fece0c3 (page 3): United Helicopters Incorporated· CC0
- 3. Hiller YH-32A (Sally Rand) helicopter gunship, US Army, 1952 - Hiller Aviation Museum - San Carlos, California - DSC03246: Daderot· CC0
what is it?
The Hiller YH-32 Hornet (company designation HJ-1) was an American ultralight helicopter built by Hiller Aircraft in the early 1950s. It was a small and unique design: it was powered by two Hiller 8RJ2B ramjet engines mounted on the rotor blade tips, which weighed 13 lb (5.9 kg) each and delivered an equivalent of 45 hp (34 kW) for a total of 90 hp (67 kW). Versions of the HJ-1 Hornet were built for the United States Army and the United States Navy in the early 1950s.
How to recognise it: 2 turboshaft engines · 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 76 years ago, in 1950.
turboshaft: A turbine that turns a shaft, usually a helicopter rotor.
spec sheet
- first flight
- 1950
- introduced
- 1954
- number built
- 18
- role
- experimental helicopter
- makers
- Hiller Aircraft Company
- engines
- 2× Hiller 8RJ2B
- crew
- 1
- passengers
- 1
- length
- 7.2 m
- rotor diameter
- 7 m
- height
- 2.4 m
- max take-off weight
- 490 kg
- top speed
- —
- cruise speed
- 111 km/h
- range
- —
- ceiling
- 2,103 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q775213, Wikipedia: Hiller YH-32 Hornet (CC BY-SA 4.0).Updated 2026-10-24.
