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Atlas XH-1 Alpha
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==Specifications (XH-1)== {{Aircraft specs |ref= |prime units?=met <!-- General characteristics --> |crew=2 |length m=10.56 |height m=2.73 |empty weight kg=1,400 |empty weight note=<ref name="jawa86p203">{{harvnb|Taylor|1986|p=203}}</ref> |max takeoff weight kg=2,200 |max takeoff weight note=<ref name="jawa86p203"/> <!-- Powerplant --> |eng1 number=1 |eng1 name=[[Turbomeca Artouste IIIB]] |eng1 type=[[turboshaft]] |eng1 kw=410 |rot number=1<!-- helicopters --> |rot dia m=11.02<!-- helicopters --> |rot area sqm=95.4<!-- helicopters --> <!-- Performance --> |max speed kmh=210 |max speed note=<ref name="jawa86p203"/> |cruise speed kmh=185 |cruise speed note=<ref name="jawa86p203"/> |climb rate ftmin=800 |climb rate note=<ref name="jawa86p203"/> |combat range km=275 |combat range note=<ref name="jawa86p203"/> <!-- Armament --> |guns= 1 Γ [[Vektor GA-1 Rattler]] 20mm cannon in a chin turret with 1,000 rounds }}
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