Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Saunders-Roe P.154 Single-Seat, Rocket-Powered Interceptor Proposal.
1 x Twin-chamber rocket motor developing a combined 8,000lb of thrust; PROPOSED: 1 x Turbojet engine (for cruising); Rocket boosters for take-off assistance.
Propulsion
1,873 mph
3,015 kph | 1,628 kts
Max Speed
60,039 ft
18,300 m | 11 miles
Service Ceiling
13,500 ft/min
4,115 m/min
Rate-of-Climb