Saturn I SA-1
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Saturn-Apollo 1 (SA-1) was the first flight of the
Saturn I The Saturn I was a rocket designed as the United States' first medium lift launch vehicle for up to low Earth orbit payloads.Terminology has changed since the 1960s; back then, 20,000 pounds was considered "heavy lift". The rocket's first sta ...
space launch vehicle, the first in the Saturn family, and first mission of the American Apollo program. The rocket was launched on October 27, 1961, from Cape Canaveral, Florida.


Objectives

The Saturn I booster was a huge increase in size and power over anything previously launched. It was three times taller, required six times more fuel and produced ten times more thrust than the
Juno I The Juno I was a four-stage American space launch vehicle, used to launch lightweight payloads into low Earth orbit. The launch vehicle was used between January 1958 to December 1959. The launch vehicle was a member of the Redstone launch ve ...
rocket that had launched the first American satellite, '' Explorer 1'', into orbit in 1958. At the time,
NASA The National Aeronautics and Space Administration (NASA ) is an independent agencies of the United States government, independent agency of the US federal government responsible for the civil List of government space agencies, space program ...
had decided to not use all-up testing, when an entire system is tested at once. The agency planned to test each rocket stage in separate launches, so for SA-1 the only live stage was the S-I first stage. This first flight was designed to test the structure of the launch vehicle during a
suborbital flight A sub-orbital spaceflight is a spaceflight in which the spacecraft reaches outer space, but its trajectory intersects the atmosphere or surface of the gravitating body from which it was launched, so that it will not complete one orbital r ...
using the nose cone from a Jupiter rocket.


Preparation

As this was the first Saturn flight, the systems were still being developed. It was the first time that a stage had been delivered to Cape Canaveral by barge and it demonstrated this could be done for the larger stages of future Saturn rockets. The first stage and the two dummy upper stages arrived on August 15, 1961, on the barge ''Compromise''. It had encountered some problems on the voyage, running aground four times due to poor
nautical chart A nautical chart is a graphic representation of a sea area and adjacent coastal regions. Depending on the scale of the chart, it may show depths of water and heights of land ( topographic map), natural features of the seabed, details of the co ...
s. On the return trip, the barge hit a bridge, causing some minor damage. The booster was erected at Pad 34 five days later with little trouble. Testing proceeded, albeit a little behind schedule. At this time, testing was not automated and amounted to flicking switches in the control center and observing how the rocket responded.


Flight

At 12:30 p.m. EST on October 27, 1961, the
RP-1 RP-1 (alternatively, Rocket Propellant-1 or Refined Petroleum-1) is a highly refined form of kerosene outwardly similar to jet fuel, used as rocket fuel. RP-1 provides a lower specific impulse than liquid hydrogen (LH2), but is cheaper, is s ...
propellant started to flow into the rocket. A slight surplus (3%) of the fuel required was put into the rocket, as it was possible to easily drain fuel. Just before launch, surplus fuel was removed from the tanks.
Liquid oxygen Liquid oxygen—abbreviated LOx, LOX or Lox in the aerospace, submarine and gas industries—is the liquid form of molecular oxygen. It was used as the oxidizer in the first liquid-fueled rocket invented in 1926 by Robert H. Goddard, an app ...
began flowing into its tanks at 3:00 a.m. the next day. It followed the same procedure as the RP-1 with the tanks being filled to 10 percent to check for leaks, then fast filled to 97 percent, then slowly topped off. Despite a couple of delays due to bad weather, the rocket was launched only one hour behind schedule. The engineers had given the rocket only a 75 percent chance of lifting off and only a 30 percent chance of completing a nominal flight. Even with a nominal flight some damage was thought possible. At the Redstone Arsenal, ground testing had shattered windows 12 km away. The sound of the launch was a disappointment for some witnesses, being described as like an
Atlas rocket Atlas is a family of US missiles and space launch vehicles that originated with the SM-65 Atlas. The Atlas intercontinental ballistic missile (ICBM) program was initiated in the late 1950s under the Convair Division of General Dynamics. Atlas was ...
launch, when observers stood 1.5 miles (2.4 km) away instead of three miles (5 km) for a Saturn launch. It was later determined that the cause of the difference between the Cape and the Redstone Arsenal was atmospheric conditions damping the sound. The flight itself was nearly perfect. The rocket reached a height of 136.5 km and impacted 345.7 km down range from the launch site in the Atlantic Ocean. The only real problem was the rocket cut off 1.6 seconds ahead of schedule. This was traced to the fact that there was 400 kg too much liquid oxygen and 410 kg too little RP-1. For the test flight, SA-1 only carried a propellant load that was 83 percent full.


References


External links

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NASA Space Science Data Coordinated Archive
{{Use American English, date=January 2014 Apollo program 1961 in spaceflight Test spaceflights Spacecraft launched by Saturn rockets