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The Keldysh bomber was a Soviet design for a rocket-powered bomber spaceplane, which drew heavily upon work carried out by Eugen Sänger and Irene Bredt for the German Silbervogel project.
In November 1946 the NII-1 NKAP research institute was formed with mathematician Mstislav Keldysh as its head to investigate and develop the German Sänger–Bredt design. In 1947, studies indicated that the high fuel consumption of Sänger's rocket-based design rendered the concept impracticable in the short term. Using engines considered to be available in a reasonable timespan, 95% of the vehicle's initial mass would have to be propellant. However, use of a rocket driven slide for the takeoff run and ramjets during the atmospheric acceleration phase would be more efficient than the original concept and could give the craft a more reasonable 22% dead weight and still achieve the 5 km·s−1 velocity required for a intercontinental range. The mission would be started using five to six rocket engines RKDS-100, burning LOX/Kerosene and driving a sled including the bomber mounted on top with a total thrust of 5 to 6 MN running on a 3 km long track. After horizontal acceleration with approximate 5 g for about 10 to 11 s up to a speed of the craft would separate and lift off, still driven by its single on-board RKDS-100 rocket engine delivering about 1 MN thrust, but now supported by two more fuel efficient wingtip mounted ramjets. After passing altitude, reaching a speed of Mach 3 and the flame out of the ramjets, the still burning rocket engine would allow leaving the atmosphere and reaching a sub-orbital flight path. It was estimated that this ambiguous development would take until the mid-1950s before a draft project of a feasible design could be prepared, and by that time the design had been made obsolete by more advanced designs. However, the work carried out lead to the EKR, MKR, Buran, and Burya ramjet cruise missiles. But when Burya reached the flight-ready status, the era of the much more powerful ICBM R-7 has already began.
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