... work has been already done on the propulsion system MAKS consists of the subsonic ... The main propulsion engine includes two RD-701 engines using three-component fuel ...
... The RD-701 is a fully integrated propulsion unit with two thrust chambers and their associated high pressure turbopumps and preburners incorporated into a thrust frame with common boost pumps, hydraulic system, and pneumatic system. ...
... a liquid propellant engine (LPE) for orbital propulsion, with the 1,500 kg/f of thrust (specific pulse of 320 sec, fuel ... a turbojet kerosene 2,000 kg/f engine with specific fuel consumption of 1.38 kg/kg*h to allow subsonic propulsion and landing. ...
... a liquid propellant engine (LPE) for orbital propulsion, with the 1,500 kg/f of thrust (specific pulse of 320 sec, fuel ... a turbojet kerosene 2,000 kg/f engine with specific fuel consumption of 1.38 kg/kg*h to allow subsonic propulsion and landing. ...
... по космическим средствам доставки и движителям (Symposium on Space Transportation and Propulsion), Мюнхен- Ottoborn, Германия ... AIAA 31-th Joint Propulsion Conference, San Diego . Доклад "Comparative Analysis of Reusable Space Transport Systems " . ...