Developed at MSFC under the direction of Dr. Wernher von Braun, the SA-5 incorporated a Saturn I, Block II engine. Launched on January 29, 1964, SA-5 was the first two stage (Block II) Saturn with orbital capability and performed the first test of Instrument Unit and successful stage separation. Block II vehicles had two live stages, and were basically in the two-stage configuration of the Saturn I vehicle. There were marked changes between the Block I and II versions. The Block II S-I stage had eight fins added for greater aerodynamic stability in the lower atmosphere. All Block II H-1 engines had a thrust of 188,000 pounds each for a combined thrust over 1,500,000 pounds. The Block II second stage (S-IV) had six RL-10 hydrogen-oxygen engines, each producing a thrust of 15,000 pounds for a total combined thrust of 90,000 pounds. A motion picture camera capsule loated on stage I was successful recovered.

The launch of the SA-5 on January 29, 1964 was the fifth Saturn I launch vehicle. The SA-5 marked a number of firsts in the Marshall Space Flight Center-managed Saturn development program, including the first flight of Saturn I Block II vehicle with eight aerodynamic fins at the bottom of the S-I stage (first stage) for enhanced stability in flight. This also was the first flight of a live S-IV (second or upper) stage with the cluster of six liquid hydrogen-fueled RL-10 engines. the first successful second stage separation, and the first use of the Launch Complex 37.

Marshall Space Flight Center (MSFC) Director Dr. Wernher von Braun (left) with Kennedy Space Center (KSC) Rocco Petrone prior to the January 29, 1964 launch of SA-5, the first Block II configuration of the Saturn I launch vehicle. Petrone played key roles at KSC in the development of Saturn launch facilities before becoming director of launch operations in 1966.

Astronaut Elliot M. See, Jr., inside Gemini Static Article (SA)-5 Spacecraft prior to Water Egress Training in the Gulf of Mexico. Astronaut See is Pilot for the Gemini-5 Backup Crew. GULF OF MEXICO

jsc2022e057892 (5/12/2022) --- The SpaceOMIX team traveling to Space Applications Services, Brussels, Belgium for sample integration [Credit: Space Applications Services, NV/SA]

jsc2022e057886 (5/12/2022) --- ICE Cubes mission control centre at the Space Applications Services, Brussels, Belgium [credit: Space Applications Services, NV/SA]

jsc2022e057891 (5/13/2022) --- A view of two samples from the onboard camera to the mission control centre and personal computer screen [Credit: Space Applications Services, NV/SA]

jsc2022e057894 (5/13/2022) --- Views of the Maltese Biocube based on the ICE Cubes platform by Belgian company Space Applications Services [Credit: Space Applications Services, NV/SA]

CLOSE-UP OF AFT END OF SATURN S-1B STAGE (SA-T) NEAR PROPULSION AND STRUCTURAL TEST FACILITY (BUILDING 4572) AT THE GEORGE C. MARSHALL SPACE FLIGHT CENTER IN HUNTSVILLE, ALABAMA.

S66-39691 (18 June 1966) --- Astronaut John W. Young, prime crew command pilot for the Gemini-10 spaceflight, sits in Static Article 5 during water egress training activity onboard the NASA Motor Vessel Retriever. The SA-5 will be placed in the water and he and astronaut Michael Collins will then practice egress and water survival techniques. At right is Gordon Harvey, Spacecraft Operations Branch, Flight Crew Support Division. Photo credit: NASA

S66-39719 (18 June 1966) --- Astronaut Michael Collins, prime crew pilot for the Gemini-10 spaceflight, sits in Static Article 5 during water egress training activity onboard the NASA Motor Vessel Retriever. The SA-5 will be placed in the water; and he and astronaut John W. Young, command pilot, will then practice egress and water survival techniques as part of their training for the planned Gemini-10 spaceflight. Photo credit: NASA

jsc2022e057883 (5/12/2022) --- A close up view of six sample cuvettes that are planned to hold five human skin tissue and microbiome samples from Diabetic Foot Ulcer patients and one yeast sample from Malta. This is part of the Follow-up Study of Human Skin Tissue Microbiome Studies and Yeast Cells in Space (Ice Cubes #9.2 – Maleth 2) investigation. Image courtesy of Space Applications Services, NV/SA.

CLOSE-UP OF H-1 ENGINE INSTALLED ON SATURN S-1B STAGE (SA-T) NEAR PROPULSION AND STRUCTURAL TEST FACILITY (BUILDING 4572) AT THE GEORGE C. MARSHALL SPACE FLIGHT CENTER.

A south tropical disturbance has just passed Jupiter's iconic Great Red Spot and is captured stealing threads of orange haze from the Great Red Spot in this series of color-enhanced images from NASA's Juno spacecraft. From left to right, this sequence of images was taken between 2:57 a.m. and 3:36 a.m. PDT (5:57 a.m. and 6:36 a.m. EDT) on April 1, 2018, as the spacecraft performed its 12th close flyby of Jupiter. Citizen scientists Gerald Eichstädt and Seán Doran created this image using data from the spacecraft's JunoCam imager. https://photojournal.jpl.nasa.gov/catalog/PIA22937 ** Image Credit: Enhanced Image by Gerald Eichstädt and Seán Doran (CC BY-NC-SA) based on images provided courtesy of NASA/JPL-Caltech/SwRI/MSSS

The Saturn I (SA-3) flight lifted off from Kennedy Space Center launch Complex 34, November 16, 1962. The third launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the direction of Dr. Wernher von Braun, incorporated a Saturn I, Block I engine. The typical height of a Block I vehicle was approximately 163 feet. and had only one live stage. It consisted of eight tanks, each 70 inches in diameter, clustered around a central tank, 105 inches in diameter. Four of the external tanks were fuel tanks for the RP-1 (kerosene) fuel. The other four, spaced alternately with the fuel tanks, were liquid oxygen tanks as was the large center tank. All fuel tanks and liquid oxygen tanks drained at the same rates respectively. The thrust for the stage came from eight H-1 engines, each producing a thrust of 165,000 pounds, for a total thrust of over 1,300,000 pounds. The engines were arranged in a double pattern. Four engines, located inboard, were fixed in a square pattern around the stage axis and canted outward slightly, while the remaining four engines were located outboard in a larger square pattern offset 40 degrees from the inner pattern. Unlike the inner engines, each outer engine was gimbaled. That is, each could be swung through an arc. They were gimbaled as a means of steering the rocket, by letting the instrumentation of the rocket correct any deviations of its powered trajectory. The block I required engine gimabling as the only method of guiding and stabilizing the rocket through the lower atmosphere. The upper stages of the Block I rocket reflected the three-stage configuration of the Saturn I vehicle. During the SA-3 flight, the upper stage ejected 113,560 liters (30,000 gallons) of ballast water in the upper atmosphere for "Project Highwater" physics experiment. The water was released at an altitude of 65 miles, where within only 5 seconds, it expanded into a massive ice cloud 4.6 miles in diameter. Release of this vast quantity of water in a near-space environment marked the first purely scientific large-scale experiment.

Colorful swirling clouds in Jupiter's North Equatorial Belt practically fill this image from NASA's Juno spacecraft. This is the closest image captured of the Jovian clouds during this recent flyby of the gas giant planet. The color-enhanced image was taken at 2:08 p.m. PDT (5:08 p.m. EDT) on Oct. 29, 2018 as the spacecraft performed its 16th close flyby of Jupiter. At the time, Juno was about 2,100 miles (3,400 kilometers) from the planet's cloud tops, at approximately 14 degrees north latitude. In other words, the spacecraft was about as close to Jupiter as San Francisco is to Chicago, which is quite close when racing over a planet that's 11 times wider than Earth. Citizen scientist Björn Jónsson created this image using data from the spacecraft's JunoCam imager. https://photojournal.jpl.nasa.gov/catalog/PIA22695. - Enhanced image by Björn Jónsson (CC-NC-SA) based on images provided courtesy of NASA/JPL-Caltech/SwRI/MSSS

This enhanced color Jupiter image, taken by the JunoCam imager on NASA's Juno spacecraft, showcases several interesting features on the apparent edge (limb) of the planet. Prior to Juno's fifth flyby over Jupiter's mysterious cloud tops, members of the public voted on which targets JunoCam should image. This picture captures not only a fascinating variety of textures in Jupiter's atmosphere, it also features three specific points of interest: "String of Pearls," "Between the Pearls," and "An Interesting Band Point." Also visible is what's known as the STB Spectre, a feature in Jupiter's South Temperate Belt where multiple atmospheric conditions appear to collide. JunoCam images of Jupiter sometimes appear to have an odd shape. This is because the Juno spacecraft is so close to Jupiter that it cannot capture the entire illuminated area in one image -- the sides get cut off. Juno acquired this image on March 27, 2017, at 2:12 a.m. PDT (5:12 a.m. EDT), as the spacecraft performed a close flyby of Jupiter. When the image was taken, the spacecraft was about 12,400 miles (20,000 kilometers) from the planet. https://photojournal.jpl.nasa.gov/catalog/PIA21389. - Enhanced image by Björn Jónsson (CC-NC-SA) based on images provided courtesy of NASA/JPL-Caltech/SwRI/MSSS

Jupiter's iconic Great Red Spot is a 10,000-mile-wide (16,000-kilometer-wide) storm that has been raging since at least the 1800s — and possibly for more than 350 years. Observations with NASA's Juno spacecraft previously indicated that the vertical extent of the Great Red Spot is over 120 miles (200 kilometers), consistent with a storm feature that develops deep in Jupiter's atmosphere. Since NASA's Voyager spacecraft visited Jupiter in 1979, the Great Red Spot has shrunk from about the size of 1.8 Earths to the size of about 1.3 Earths today. NASA's Juno spacecraft has imaged the Great Red Spot numerous times, providing unique information on the details of how the Great Red Spot dynamically changes while it is shrinking. This montage includes five map-projected mosaics of the giant storm, processed from images obtained by the JunoCam imager during several orbits between July 2017 and July 2019. The mosaics show how the Great Red Spot and nearby areas have changed over the course of the Juno mission. Will the Great Red Spot continue to shrink? Only time will tell, but as we study Jupiter's atmosphere, we learn more about how weather systems work, both on giant planets such as Jupiter and Saturn and also on our own home, Earth. Citizen scientist Björn Jónsson created this montage using JunoCam data. The images cover latitudes from about 5 degrees to 38 degrees south. Enhanced image by Björn Jónsson (CC-NC-SA) based on images provided courtesy of NASA/JPL-Caltech/SwRI/MSSS