MAKS-D
Winged orbital launch vehicle. Year: 1993. Family: Air-Launched. Country: Russia. Status: Study 1981.

NPO Molniya, Antonov, and TsAGI proposed a spaceplane demonstrator project to the European Space Agency in 1993-1994 under the RADEM project. This would be a scaled-back version of the cancelled MAKS spaceplane using existing rocket engines. An unmanned prototype of the MAKS would be fitted out with RD-120 Lox/Kerosene engines. Launched from atop the An-225, the MAKS-D would reach an altitude of 80 to 90 km and a speed of Mach 14 to 15.

The ES experimental spacecraft would have a launch mass of 56 metric tons, including 45 metric tons of propellant. It would fly at hypersonic speed out to a range of 1500 km, and then return to an automatic landing at its launching base. Three variants were proposed:

  • Basic variant. Purpose of the flight tests would be to prove MAKS-M / I-HOTOL flight algorithms, materials, and engine reusability. 38.0 m length x 24.0 m wingspan

  • Basic variant modified for scramjet flight tests

  • Orbital vehicle with 2 metric tons payload. For the orbital vehicle the MAKS-D served as the first stage of the booster. It would release the RS rocket stage, equipped with a European HM-7B Lox/LH2 engine. The rocket stage engine would ignite five seconds after release of the aircraft from the An-225 transport and work in tandem with the RD-120 installed on MAKS-D. Following exhaustion of main stage propellants the MAKS would release the rocket stage, which would continue on to orbit. This scheme was analogous to NASA's early X-34 concepts.

Manufacturer: Molniya. LEO Payload: 2,000 kg (4,400 lb). to: 200 km Orbit. at: 51.00 degrees. Total Mass: 185,000 kg (407,000 lb).



MAKS-D Chronology

1993 - Launch Vehicle: MAKS-D.

  • RADEM project Nation: Russia. NPO Molniya, Antonov, and TsAGI proposed a spaceplane demonstrator project to the European Space Agency in 1993-1994 under the RADEM project. This would be a scaled-back version of the cancelled MAKS spaceplane using existing rocket engines.

Bibliography and Further Reading
  • Lozino-Lozinskiy, G E, editor, Aviationno-kosmicheskiye sistemy, MAI, Moscow, 1997. ISBN: 5703520681. Russian language collection of technical papers that cover the design, development, engineering, and flight test results of the BOR-4, BOR-5, Buran, and MAKS spaceplanes. Includes intermediate designs More at amazon.com...
 
 
 
 
 
 
 
 
 

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