Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Heinkel He P.1077 (Julia) Rocket-Powered Interceptor Aircraft Proposal.
1 x Walter HWK 509C liquid-fuel rocket motor developing 3,750lb of thrust; 4 x Schmidding 533 jettisonable booster rockets developing 2,650lb of thrust each during take-off.
Propulsion
559 mph
900 kph | 486 kts
Max Speed
49,213 ft
15,000 m | 9 miles
Service Ceiling
40 miles
64 km | 35 nm
Operational Range
39,400 ft/min
12,009 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).