Developed by Rocketdyne, the F-1 engine generated nearly 1.5 million pounds of thrust. F-1 engines were clustered in groups of five in the first stage (S-IC stage) of Saturn V rockets. As a group, the five engines gulped 15 tons of kerosene and Liquid oxygen per second.
(Photos: Richard Kruse, 2002)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
The H-1 was developed by Rocketdyne and used kerosene and liquid oxygen as propellents. Eight H-1 engines were used on the first stage of Saturn I and IB rockets.
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
The J-2 was developed by Rocketdyne and used liquid hydrogen and liquid oxygen as propellents. The Saturn 5 second stage (S-II) used five J-2 engines, while the third stage (SIV-B) used a single J-2.
(Photos: Richard Kruse, 2002)
(Photos: Richard Kruse, 2007)
The LR-87 rocket was used on Titan missiles and space launchers.
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2002)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
The S-3 rocket was used on the Thor and Jupiter rockets. The military designation for the S-3 was LR-79.
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
The Space Shuttle Main Engine (SSME) was developed in Huntsville, Alabama at the Marshall Space Flight Center. The SSME uses liquid hydrogen and liquid oxygen as propellents. The Space Shuttle uses three SSME.
(Photos: Kevin Reynolds, 2000)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2009)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
The XLR-11 was developed to propel manned rocketplanes. This four-chambered rocket engine used alcohol and liquid oxygen as propellent.
(Photos: Richard Kruse, 2007)
The XLR-99 was used in the X-15 hypersonic rocketplane. The XLR-99 used ammonia and liquid oxygen as propellent.
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2007)
(Photos: Richard Kruse, 2002)
(Photos: Richard Kruse, 2008)
(Photos: Richard Kruse, 2008)
Images by Richard Kruse are licensed under a Creative Commons Attribution-Noncommercial 3.0 United States License.