Aerojet 260

Aerojet 260 motor test, 25 September 1965

The Aerojet 260 was an experimental solid rocket motor constructed and tested in the mid-1960s by Aerojet for NASA.[1][2][3][4]

  1. ^ Baker, J. (1978-07-25). "Methods used for Space Shuttle SRB thrust shape design". 14th Joint Propulsion Conference. Las Vegas, NV, U.S.A.: American Institute of Aeronautics and Astronautics. doi:10.2514/6.1978-986.
  2. ^ Andrepont, Wilbur; Felix, Rafael (1994-06-27). "The History of Large Solid Rocket Motor Development in the United States". 30th Joint Propulsion Conference and Exhibit. Indianapolis, IN, U.S.A.: American Institute of Aeronautics and Astronautics. doi:10.2514/6.1994-3057.
  3. ^ Hall, A. M.; Slunder, C. J. (1968). The Metallurgy, Behavior, and Application of the 18-Percent Nickel Maraging Steels (NASA SP-5051). NASA.
  4. ^ Crimmins; Cousineau; Rogers; Shell (June 1999). "THE 260 - The Largest Solid Rocket Motor Ever Tested" (PDF). 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.