The Saturn I was a rocket designed as the United States' first medium lift launch vehicle for up to 20,000-pound (9,100 kg) low Earth orbit payloads. The rocket's first stage was built as a cluster of propellant tanks engineered from older rocket tank designs, leading critics to jokingly refer to it as "Cluster's Last Stand". Its development was taken over from the Advanced Research Projects Agency (ARPA) in 1958 by the newly formed civilian NASA. Its design proved sound and flexible. It was successful in initiating the development of liquid hydrogen-fueled rocket propulsion, launching the Pegasus satellites, and flight verification of the Apollo command and service module launch phase aerodynamics. Ten Saturn I rockets were flown before it was replaced by the heavy lift derivative Saturn IB, which used a larger, higher total impulse second stage and an improved guidance and control system. It also led the way to development of the super-heavy lift Saturn V which carried the first men to landings on the Moon in the Apollo program.
A 1/20th-scale model of first-stage Saturn is prepared for testing in the 16-foot transonic wind tunnel at Arnold Air Force Base in the early 1960s
Von Braun, with JFK pointing at Saturn I at Cape Canaveral on 16 November 1963, weeks prior to its launch
Diagram of the S-I first stage of the Saturn I
Rocketdyne was an American rocket engine design and production company headquartered in Canoga Park, in the western San Fernando Valley of suburban Los Angeles, in southern California.
Rocketdyne, former main production facility in Canoga Park, Los Angeles.
Rocketdyne's test stand for testing the J-2 engine in Santa Susana Mountains
Aerial view of Rocketdyne Canoga Plant in 1960. View is to the south east. The intersection of Owensmouth and Vanowen streets is seen at lower right while the intersection of Canoga and Victory streets is seen towards the upper center, nearby the multi-story headquarters building.
Static display of a Lockheed F-104G aircraft in German National livery fitted with a Rocketdyne zero length launch rocket engine.