This page no longer updated from 31 October 2001. Latest version can be found at Star 26B

Star-26B -

Credit: Thiokol. 2,229 bytes. 110 x 89 pixels.

Manufacturer Name: TE-M-442-1. Government Designation: Burner 2A. Other Designations: 17.8-KS-7,784. Designer: Thiokol. Gross Mass: 261 kg. Empty Mass: 23 kg. Propellants: Solid Thrust(vac): 3,531 kgf. Isp: 272 sec. Burn time: 18 sec. Diameter: 0.7 m. Chambers: 1. Country: USA. Status: In Production. References: 410 . Comments: Upper stage motor was flown on the Burner IIA spacecraft for Boeing and the U.S. Air Force. Total flown included in total for Star-26C. Total impulse 64,731 kgf-sec. Motor propellant mass fraction 0.91.
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 .