Nakajima G10N: Perbedaan antara revisi
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Baris 10:
Proyek ini disusun oleh kepala Nakajima Chikuhei Nakajima. Desainnya memiliki sayap lurus dan [[Baling-baling berputar|baling-baling]] empat bilah [[Baling-baling berputar|kontra-berputar]]. Untuk menghemat berat, beberapa [[roda pendaratan]] harus dibuang setelah lepas landas (karena tidak perlu mendarat dengan muatan bom yang dikosongkan), seperti yang telah direncanakan pada beberapa desain yang setara dalam program ''[[Amerikabomber]]'' yang dikembangkan Jerman. Pesawat itu menggunakan enam mesin,<ref name="Dyer4">{{Cite book|last=Dyer|first=Edwin M. III|title=Japanese Secret Projects:Experimental aircraft of the IJA and IJN 1939–1945|url=https://archive.org/details/japanesesecretpr00dyer|publisher=Midland publishing|location=Hinkley|year=2009|edition=1st|pages=[https://archive.org/details/japanesesecretpr00dyer/page/n57 108]–111|isbn=978-1-85780-317-4}}</ref> seperti desain ''Amerika Bomber'' di kemudian hari, untuk mengkompensasi [[Luftwaffe|output mesin pesawat Jerman yang dibatasi hingga maksimum 1.500 kW (2.000 hp)]].<ref>{{Cite book|last=Griehl|first=Manfred|last2=Dressel|first2=Joachim|title=Heinkel He 177 - 277 - 274|url=|access-date=|year=1998|publisher=Airlife Publishing|location=Shrewsbury, UK|isbn=1-85310-364-0|page=188}}</ref>
Pembangunan dimulai pada Januari 1943, dengan desain dan fasilitas manufaktur yang dibangun di [[Mitaka|Mitaka, Tokyo]]. Mesin Nakajima 36 silinder 5.000
Proyek Z dibatalkan pada Juli 1944, dan ''Fugaku'' tidak pernah diproduksi.<ref name="Dyer5">{{Cite book|last=Dyer|first=Edwin M. III|title=Japanese Secret Projects:Experimental aircraft of the IJA and IJN 1939–1945|publisher=Midland publishing|location=Hinkley|year=2009|edition=1st|pages=108–111|isbn=978-1-85780-317-4}}</ref>
Baris 25:
General characteristics
-->|crew=6 to 10<br/>
::::'''Fugaku:''' 7 to 8|length m=44.98|length note=
::::'''Fugaku:''' {{convert|39.98|m|ft|abbr=on|0}}|span m=64.98|span note=
::::'''Fugaku:''' {{convert|62.97|m|ft|abbr=on|0}}|height m=8.77|wing area sqm=352.01|wing area note=
::::'''Fugaku:''' {{convert|330|m2|sqft|abbr=on|2}}|aspect ratio=12.1|empty weight kg=65,000|empty weight note=
::::'''Fugaku:''' {{convert|33,800|kg|lb|abbr=on|2}}|gross weight kg=122,000|gross weight note=
::::'''Fugaku:''' {{convert|42,000|kg|lb|abbr=on|2}}|max takeoff weight kg=160,000|max takeoff weight note=
::::'''Fugaku:''' {{convert|70,000|kg|lb|abbr=on|2}}
<!--
Powerplant
-->|eng1 number=6|eng1 name=[[Nakajima Ha-54]]|eng1 type=36-cyl. air-cooled radial piston engines|eng1 hp=5,000<!-- prop engines -->|eng1 note=at take-off<br/>
::::'''Fugaku:''' 6x [[Nakajima NK11A]] 18-cyl. air-cooled radial piston engines developing {{convert|2,500|hp|kW|abbr=on|0}} at take-off|prop blade number=6<!-- propeller aircraft -->|prop name=contra-rotating constant speed propellers|prop dia m=4.5<!-- propeller aircraft -->|prop dia note=
::::'''Fugaku:''' 4-bladed constant speed propellers {{convert|4.8|m|ft|abbr=on|0}} diameter
<!--
Performance
-->|max speed kmh=679|max speed note=at {{convert|10,000|m|ft|abbr=on|0}}<br/>
::::'''Fugaku:''' {{convert|779|km|mi|abbr=on|0}}at {{convert|10,000|m|ft|abbr=on|0}}|max speed mach=<!-- supersonic aircraft -->|range km=17,999|range note=maximum
::::'''Fugaku:''' {{convert|19,400|km|mi|abbr=on|0}}|ceiling m=15,000|wing loading kg/m2=456.99|wing loading note=
::::'''Fugaku:''' 211.89 m² (43.4 lb/ft²)|power/mass=0.103 kW/kg (0.063 hp/lb)
::::'''Fugaku:''' 0.118 kW/kg (0.07 hp/lb)
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