This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Saenger II

Saenger 2 Spaceplane
Saenger 2 Spaceplane

Credit: Mark Lindroos. 15,301 bytes. 470 x 179 pixels.


Family: Winged. Country: Germany. Status: Study 1985.

Proposed two stage to orbit vehicle. Air-breathing hypersonic first stage and delta wing second stage. The German Hypersonics Programme and its Saenger II reference vehicle received most of the domestic funding for spaceplane development in the late 1980s and early 1990s. Saenger II comprised a large hypersonic booster aircraft capable of Mach 4 cruise plus a small rocket-powered upper stage (HORUS) that could deliver people and cargo to low Earth orbit. The booster aircraft (to be powered by turboramjets) was designed for maximum commonality with a supersonic passenger transport (with. a cruise range of 11,000km). Development would have been very costly and the programme was cancelled in 1994.



Saenger 2 SpaceplaneSaenger 2 Spaceplane

Credit: Mark Lindroos. 26,168 bytes. 393 x 361 pixels.


Specifications

Liftoff Thrust: 458,870 kgf. Total Mass: 366,000 kg. Core Diameter: 14.0 m. Total Length: 101.0 m. Flyaway Unit Cost $: 28.00 million. in 1985 unit dollars.



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .