International Space Station Outlines

Vector line drawings of the International Space Station from different perspectives, emphasizing structural details in a technical style.

International Space Station Outline. Vector

S63-19317 (October 1963) --- Pen and ink views of comparative arrangements of several capsules including the existing Big Joe design, the compromise Big Joe design, and the Little Joe . All capsule designs are labeled and include dimensions.

Four-cycle principle of an engine, illustration

A model of the Multi-purpose Chemical Laser. Country: Unknown

S64-01123 (1964) --- Artist concept illustrating the relative sizes of the one-man Mercury spacecraft, the two-man Gemini spacecraft, and the three-man Apollo spacecraft.

Tu-95 Bear

Defense air gun isometric war vector Pakistan day soldier military white isolated

Artist Carter Emmart 'The Case for Mars' conference artwork (Mission to Mars) NOTE; for government educational use only -

Milk pump with pounded milk milk pump with pounded milk copyright: xzoonar.com/DR.XNORBERBERTXLANGEX 14449649

Evangelista Torricelli's (1608-1647) demonstration 1643. It showed that the height of a column of liquid is governed by atmospheric pressure and that the height of the column is directly proportional to the density of the liquid. Water will rise to 9.75m (32 feet) but mercury, which is approximately 13.5 times denser, will only rise to .736m (29 ins). A meter (3 feet) tube is filled with mercury and the open end placed in a dish of mercury. The liquid will fall in the tube until the weight of the column is in equilibrium with atmospheric pressure - .736m (29 ins). From 'The Atmosphere' by Camille Flammarion. (London, 1873).

Diatom found in pond water near Grant, NY. USA. Magnification 400x

Artist's rendering of the Orion Artemis I spacecraft.

JSC2003-E-42547 (For Release 18 June 2003) --- This graphic shows the Kibo Japanese Experiment Module (JEM) Remote Manipulator System (RMS). The RMS is used to exchange experiment payloads or hardware located on the JEM Exposed Facility and Experiment Logistics Module - Exposed Section and from inside the Pressurized Module through a scientific airlock, support maintenance tasks of Kibo and handle orbital replacement units (ORUs). The Main Arm can handle up to seven tons (14,000 pounds) of hardware and the Small Fine Arm, when attached to the Main Arm, handles more delicate operations.

An illustration of MOXIE (Mars Oxygen ISRU Experiment) and its components. An air pump pulls in carbon dioxide gas from the Martian atmosphere, which is then regulated and fed to the Solid OXide Electrolyzer (SOXE), where it is electrochemically split to produce pure oxygen.

$Engraving depicting William Huggins' stellar spectroscope which he used on his 8-inch diameter refractor at Tulse Hill. Constructed by Browning of London, the relative positions of telescope and prisms could be adjusted by a Micrometer screw so that different parts of the spectrum could be examined. William Huggins (1824-1910) an English astronomer best known for his pioneering work in astronomical spectroscopy together with his wife Margaret Lindsay Huggins. Dated 19th century$

Illustration of an astronaut

Bathyscaphe with Ecuadorian flag. Marine geology, oceanography in Ecuador, 3D rendering Bathyscaphe with Ecuadorian flag. Marine geology, oceanography in Ecuador, 3D rendering isolated on white background Copyright: xZoonar.com/natatravelx 22994525

These schematic drawings show a top view and a cutaway view of a section of the drill on NASA's Curiosity rover on Mars.

S71-16823 (January 1971) --- A line drawing illustrating a cutaway view of the Apollo 14 Command and Service Modules, showing the engineering changes in the CSM which were recommended by the Apollo 13 Review Board. (The Apollo 13 abort was caused by a short circuit and wiring overheating in one of the SM cryogenic oxygen tanks.) The major changes to the Apollo 14 CSM include adding a third cryogenic oxygen tank installed in a heretofore empty bay (in sector one) of the SM, addition of an auxiliary battery in the SM as a backup in case of fuel cell failure, and removal of destratification fans in the cryogenic oxygen tanks and removal of thermostat switches from the oxygen tank heater circuits. Provision for stowage of an emergency five-gallon supply of drinking water has been added to the CM.

This engineering drawing shows the five devices that make up the turret at the end of the arm on NASA's Curiosity rover. These include: the drill for acquiring powdered samples from interiors of rocks.

Yellow telescope

Mechanical engineering drawings on blue background. Boring bar with micrometric adjustment. Technical Design. Cover. Blueprint. Vector illustration.

Apollo Spacecraft Configured for Apollo-Soyuz Mission

3d printing of human brain isometric composition on white background vector illustration. Human Organs Isometric Composition

Scientists have now named the four marks near NASA's Curiosity rover where blasts from the descent stage rocket engines blew away some of the Martian surface material. Clockwise from the most north: Burnside, Goulburn, Hepburn and Sleepy Dragon.

This graphic shows the location of four cameras and a microphone on the spacecraft for NASA's Mars 2020 Perseverance mission. These cameras will capture the entry, descent, and landing phase of the mission.

This artist's rendering shows NASA's Voyager spacecraft. Voyager 2 was launched on Aug. 20, 1977. Voyager 1 was launched on Sept. 5, 1977.

Switzerland, Geneva, Miniature of ATLAS Detector in CERN. Miniature of the ATLAS Detector. CERN, the European Organization for Nuclear Research, is the biggest particle physics laboratory in the world.

Mechanical engineering drawings on black background. Milling machine spindle. Technical Design. Cover. Blueprint. Vector illustration. Mechanical engineering drawings on black background. Milling machine spindle. Technical Design. Cover. Blueprint.

Jackhammer, pneumatic drill visualization 3d cad model, blueprint. 3D rendering Jackhammer, pneumatic drill visualization 3d cad model, blueprint. 3D rendering Copyright: xZoonar.com/natatravelx 22997385

Hand drawn space objects. Planets, comets, rockets.Vector sketch illustration.. Space objects. Planets, comets, rockets.Sketch illustration.

Line drawing depicts the location of one of three racks that will make up the Materials Science Research Facility in the U.S. Destiny laboratory module to be attached to the International Space Station (ISS). Other positions will be occupied by a variety of racks supporting research in combustion, fluids, biotechnology, and human physiology, and racks to support lab and station opertions. The Materials Science Research Facility is managed by NASA's Marshall Space Flight Center.

Mechanical engineering drawings on blue background. Broach. Technical Design. Cover. Blueprint. Vector illustration. Mechanical engineering drawings on blue background. Broach. Technical Design. Cover. Blueprint. Vector illustration.

Telescope isolated on white background for search star universe, science concept

Telescope isolated on white background for search star universe, science concept

Data analysis. Market concept with pencil drawing graphs and diagrams

Rocket Blueprint Cartoon

Rocket Blueprint Cartoon

Scanning electron microscope control panel, illustration

This engineering drawing shows various components needed to support tools at the end of the arm on NASA's Curiosity rover, including: calibration targets for helping instruments set their baseline levels.

This drawing depicts one set of flow patterns simulated in the Geophysical Fluid Flow Cell (GFFC) that flew on two Spacelab missions. Silicone oil served as the atmosphere around a rotating steel hemisphere (dotted circle) and an electrostatic field pulled the oil inward to mimic gravity's effects during the experiments. The GFFC thus produced flow patterns that simulated conditions inside the atmospheres of Jupiter and the Sun and other stars. The principal investigator was John Hart of the University of Colorado at Boulder. It was managed by NASA's Marshall Space Flight Center (MSFC). An Acrobat PDF copy of this drawing is available at http //microgravity.nasa.gov/gallery. (

Soyuz Spacecraft

Skiopticon image from the Department of Photography at the Royal Institute of Technology. Use by Professor Helmer Bäckström as lecture material. Bäckström was Sweden's first professor in photography at the Royal Institute of Technology in Stockholm 1948-1958.Tråtgången in microscopes. For more info see: Photographic yearbook in 1947.

This illustration shows the docking configuration of the Apollo-Soyuz Test Project (ASTP). The ASTP was the first international docking of the U.S.'s Apollo spacecraft and the U.S.S.R.'s Soyuz spacecraft in space. A joint engineering team from the two countries met to develop a docking system that permitted the two spacecraft to link in space and allowed the two crews to travel from one spacecraft to the other. This system entailed developing a large habitable Docking Module (DM) to be carried on the Apollo spacecraft to facilitate the joining of two dissimilar spacecraft. The Marshall Space Flight Center was responsible for development and sustaining engineering of the Saturn IB launch vehicle during the mission. The ASTP marked the last use of the Saturn Launch Vehicle.

This illustration depicts a configuration of the Command Service Module (CSM) and Docking Module (DM) for the Apollo-Soyuz Test Project (ASTP). The ASTP was the first international docking of the U.S.'s Apollo spacecraft and the U.S.S.R.'s Soyuz spacecraft in space. A joint engineering team from the two countries met to develop a docking system that permitted the two spacecraft to link in space and allowed the two crews to travel from one spacecraft to the other. This system entailed developing a large habitable Docking Module (DM) to be carried on the Apollo spacecraft to facilitate the joining of two dissimilar spacecraft. The Marshall Space Flight Center was responsible for development and sustaining engineering of the Saturn IB launch vehicle during the mission. The ASTP marked the last use of the Saturn Launch Vehicle.

S65-05399 (1965) --- Composite drawing showing the vertical, lateral, forward and aft maneuvering control of the Gemini spacecraft.

Planetary rover with five golden stars, 3D rendering Planetary rover with five golden stars, 3D rendering isolated on white background Copyright: xZoonar.com/alexlmxx 23001858

Facility Aerodynamic Validation and Operational Research (FAVOR) aircraft model hardware in 8x6 Supersonic Wind Tunnel (SWT)

The ISRU Pilot Excavator digs its way through the regolith bin during testing inside Swamp Works at NASAs Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

jsc2019e039822 (7/16/2019) --- A CAD image showing the structure of the bioreactor in the BioRock experiment.The two culture chambers are visible and the body of the unit, which contains media and fixative. (Image Courtesy of: ESA)

The genealogical tree

A photograph showing bombs at the Aviatioal Experimental Station in Hampton, VA during World War One. The photo was taken on July 22, 1917. The description indicates that the bombs have the symbol "3334", and additional notes indicate their purpose.

Human Sperm cell structure diagram, 3d rendering

Facility Aerodynamic Validation and Operational Research (FAVOR) aircraft model hardware in 8x6 Supersonic Wind Tunnel (SWT)

S69-34072 (May 1969) --- Artist's drawing illustrating a cutaway view of the Command and Service Modules of the Apollo 10 lunar orbit mission. Arrows point to various components and features of the CSM.

This schematic details the third High Energy Astronomy Observatory (HEAO)-3. The HEAO-3's mission was to survey and map the celestial sphere for gamma-ray flux and make detailed measurements of cosmic-ray particles. It carried three scientific experiments a gamma-ray spectrometer, a cosmic-ray isotope experiment, and a heavy cosmic-ray nuclei experiment. The HEAO-3 was originally identified as HEAO-C but the designation was changed once the spacecraft achieved orbit.

The Saturn V vehicle, carrying the unmarned orbital workshop for the Skylab-1 mission, lifted off successfully and all systems performed normally. Sixty-three seconds into the flight, engineers in the operation support and control center saw an unexpected telemetry indication that signalled that damages occurred on one solar array and the micrometeoroid shield during the launch. The micrometeoroid shield, a thin protective cylinder surrounding the workshop protecting it from tiny space particles and the sun's scorching heat, ripped loose from its position around the workshop. This caused the loss of one solar wing and jammed the other. Still unoccupied, the Skylab was stricken with the loss of the heat shield and sunlight beat mercilessly on the lab's sensitive skin. Internal temperatures soared, rendering the station uninhabitable, threatening foods, medicines, films, and experiments. This image, taken during a fly-around inspection by the Skylab-2 crew, shows the station's remaining

This 1968 cutaway drawing illustrates the Saturn IB launch vehicle with its two booster stages, the S-IB and S-IVB. Developed by the Marshall Space Flight Center (MSFC) as an interim vehicle in MSFC's building block approach to the Saturn rocket development, the Saturn IB utilized Saturn I technology to further develop and refine the larger boosters and the Apollo spacecraft capabilities required for the marned lunar mission.

This 1973 chart details Skylab's Ultraviolet (UV) Spectrograph, an Apollo Telescope Mount instrument. Its telescope, with camera and TV capability, photographed the Sun in selected ultraviolet wavelengths. The spectrograph was used to record the spectrum of UV emissions, such as flares or filaments, from a small individual feature on the solar disc. Real-time TV was used by the crew to monitor performance of the telescope, transmit to the ground and record. The exposed films were retrieved by astronaut extravehicular activities. The Marshall Space Flight Center had program management responsibility for the development of the Skylab hardware and experiments.

TERMINATOR SALVATION (2009), directed by MCG.

Chart showing Soviet and U.S. fourth generation intercontinental ballistic missiles. "Soviet Military Power," 1983, Pages 20. Country: Unknown

Berger Geodetic Level, Engineering - Surveryor's Instruments

Space rocket launchers developed since the 1950s. Dated 20th Century

Illustration showing new U.S. and Soviet space launch vehicles. "Soviet Military Power," 1983, Page 68. Country: Unknown

This cutaway drawing shows the S-IVB stage in its Saturn IB configuration. As a part of the Marshall Space Flight Center's (MSFC) building block approach to the Saturn development, the S-IVB stage was utilized in the Saturn IB launch vehicle as a second stage and, later, the Saturn V launch vehicle as a third stage. The stage was powered by a single J-2 engine, initially capable of 200,000 pounds of thrust.

This cutaway illustration shows the Saturn V S-II (second) stage with callouts of major components. When the Saturn V first stage burns out and drops away, power for the Saturn was provided by the S-II (second) stage with five J-2 engines which produced a total of 1,150,000 pounds of thrust. Four outer engines are placed in a square pattern with gimbaling capability for control and guidance, with the fifth engine fixed rigidly in the center.

This graphic shows the times at which NASA's Curiosity rover hit its milestones during its entry, descent and landing on Mars. Times the events actually occurred are in red; times that Earth received confirmation that events occurred appear in blue.

Chart showing Soviet and U.S. nuclear-powered ballistic missile submarines and missiles. "Soviet Military Power," 1983, Pages 22. Country: Unknown

Cutaway drawing showing an instrument of the international ionosphere satellite (S-51), the first of the three satellites in the co-operative international programme being conducted by the United Kingdom and the United States. Dated 20th century

Venous access port, illustration

Abstract mash line and point Oil pipeline. Petroleum fuel industry transportation line connection dots blue vector illustration

Nuclear Bomb Weapon Clipart Vector

An artist's concept of the receiver and transmitter of the Soviet large phased-array ballistic missile detection and tracking radar at Pechora. Country: Unknown

Artist Concepts, Apollo Mission S66-10983 Ascent Stage Liftoff (S66-05094) S66-10984 Orientation During Ascent Phase (S66-05098) S66-10985 Midcourse Coast (S66-05113) S66-10986 Survey of Landing Site (S66-05117) S66-10987 Lunar Module (LM) Jettison (S66-05089) S66-10988 Trans-Earth Injection (S66-05090) S66-10989 Exploration on Lunar Surface Apollo Surface Lunar Exploration Experiment (ASLEP) S66-10990 Liftoff (S66-05125) S66-10991 Command Module (CM)-Service Module (SM) Separation (S66-05101 N/F) S66-10992 Touchdown on Lunar Surface (S66-05115) S66-10993 Transfer Orbit Insertion (S66-05111) S66-10994 Drogue Parachute Deployment S66-10995 S-IC Stage Separation S-II Stage Thrusting (S66-05099) S66-10996 Jettison Launch Escape System (S66-05114) S66-10997 Main Parachute Deployment (S66-05091) S66-10998 Mid-course correction (S66-05088) S66-10999 Lunar Orbit Insertion (S66-05086) S66-11000 Command Service Module (CSM)-LM Docked in LM Adapter-S-IVB (S66-06526) S66-11001 Docking and Separat

This illustration is a schematic of the High Energy Astronomy Observatory (HEAO)-2 and its experiments. It shows the focal plane instruments (at the right) plus the associated electronics for operating the telescope as it transmitted its observations to the ground. A fifth instrument, the Monitor Proportional Counter, is located near the front of the telescope. Four separate astronomical instruments are located at the focus of this telescope and they could be interchanged for different types of observations as the observatory pointed at interesting areas of the Sky. Two of these instruments produced images; a High Resolution Imaging Detector and an Imaging Proportional Counter. The other two instruments, the Solid State Spectrometer and the Crystal Spectrometer, measured the spectra of x-ray objects. A fifth instrument, the Monitor Proportional Counter, continuously viewed space independently to study a wider band of x-ray wavelengths and to examine the rapid time variations in the sou

Berger Engineers' 18 Inch Wye Level, Engineering - Surveryor's Instruments

First Arcas meteorological rocket, shown at Wallops prior to flight test, July 31, 1959. Photograph published in A New Dimension Wallops Island Flight Test Range: The First Fifteen Years by Joseph Shortal. A NASA publication. Page 696.

S69-34498 (May 1969) --- Labeled artist's concept of Apollo Applications Program (AAP) Skylab Cluster.

Moscow Ballistic Missile Defense. Country: Unknown

A chart comparing U.S. and Soviet tactical surface-to-air missile characteristics. Country: Unknown

Characteristics of primary U.S. and Soviet theater missiles. Country: Unknown

Multipurpose aerospace system Buran

Artist's concept of the Mark 12A re-entry vehicle. Country: Unknown

A861082 HORZONTAL TEST BED LOS DRAWING EDWARDS (Project Engineer) SEP 25 1986 EG&G/NTS PHOTO LAB Publication Date: 9/25/1986 DRAWINGS; EDGERTON, GERMESHAUSEN & GRIER; EDWARDS, BOBBY G.; EG&G; HORIZONTAL TEST BED; ILLUSTRATIONS; LINE OF SIGHT; LOS DRAWING; NEVADA; NEVADA TEST SITE; NTS; NUCLEAR ENERGY TECHNOLOGY; NUCLEAR TESTING; NUCLEAR TESTS; TEST CHAMBERS; TEST SITES; TUNNELS; UGT; UNDERGROUND; UNDERGROUND TESTING; WEAPONS EFFECTS; WEAPONS TECHNOLOGY historical images. 1972 - 2012. Department of Energy. National Nuclear Security Administration. Photographs Related to Nuclear Weapons Testing at the Nevada Test Site.

This cutaway illustration shows the Apollo Spacecraft with callouts of the major components. The spacecraft consisted of the lunar module, the service module, the command module, and the launch escape system.

Mechanical engineering drawings on light background. Milling machine spindle. Technical Design. Cover. Blueprint. Vector illustration.. Mechanical engineering drawings on light background. Milling machine spindle. Technical Design. Cover. Blueprint

Atomic Energy - Problems Of International Control.Timing And Sequence - U.S.S.R. Outlaw weapons First - then establish United Nations control system. April 12, 1949. (Photo by Official United Nations).

The Apollo 11 mission launched from the Kennedy Space Center (KSC) in Florida via the Marshall Space Flight Center (MSFC) developed Saturn V launch vehicle on July 16, 1969 and safely returned to Earth on July 24, 1969. Aboard the space craft were astronauts Neil A. Armstrong, commander; Michael Collins, Command Module (CM) pilot; and Edwin E. (Buzz) Aldrin Jr., Lunar Module (LM) pilot. With the success of Apollo 11, the national objective to land men on the Moon and return them safely to Earth had been accomplished. These sketches illustrate four events of the Apollo 11 spacecraft and crew enroute to the Moon. Panels housing the LM were jettisoned and the CM turned 180 degrees in the transposition maneuver. The CM docked with the LM and extracted it from the third stage instrument unit of the Saturn V launch vehicle. Astronauts performed navigation checks enroute to the moon. The service propulsion system was fired to slow the spacecraft and permitted it to enter lunar orbit.

Wake Vortex behind a helicopter describing Longitudinal Cores (Secondary Vortes Generation) from Aviatsiya / Kosmonautika, 1973 (Illustration)

This image illustrates the basic differences between the three Saturn launch vehicles developed by the Marshall Space Flight Center. The Saturn I, consisted of two stages, the S-I (eight H-1 engines) and the S-IV (six RL-10 engines). The Saturn IB (center) also consisted of two stages, the S-IB (eight H-1 engines) and the S-IVB (one J-2 engine). The Saturn V consisted of three stages, the S-IC (five F-1 engines), the S-II (five J-2 engines), and the S-IVB (one J-2 engine).

The Saturn V vehicle, carrying the unmarned orbital workshop for the Skylab-1 mission, lifted off successfully and all systems performed normally. Sixty-three seconds into flight, engineers in the operation support and control center saw an unexpected telemetry indication that signalled that damages occurred on one solar array and the micrometeoroid shield during the launch. The micrometeoroid shield, a thin protective cylinder surrounding the workshop protecting it from tiny space particles and the sun's scorching heat, ripped loose from its position around the workshop. This caused the loss of one solar wing and jammed the other. Still unoccupied, the Skylab was stricken with the loss of the heat shield and sunlight beat mercilessly on the lab's sensitive skin. Internal temperatures soared, rendering the station uninhabitable, threatening foods, medicines, films, and experiments. This image, taken during a fly-around inspection by the Skylab-2 crew, shows the damaged meteoroid shield

CAPE CANAVERAL, Fla. -- This diagram of a space shuttle orbiter shows the location of avionics bay 5. Space shuttle Endeavour was scheduled to launch on the STS-134 mission to the International Space Station on April 29, but that attempt was scrubbed to allow engineers to assess an issue associated with failed heaters on a fuel line for Endeavour's auxiliary power unit-1 (APU-1). STS-134 will be the final spaceflight for Endeavour.

DD-ST-85-06537. Country: Unknown

A cutaway illustration of Saturn I launch vehicle characteristics The Saturn I, first of the Saturn launch vehicles' family, is a two-stage vehicle with a low-earth-orbit payload capability of approximately 25,000 pounds. The research and development program was plarned in two phases or blocks; one for first stage development (Block I) and the second for first and second stage development (Block II). The S-I (first) stage consisted of a cluster of nine propellant tanks and eight H-1 engines built by Rocketdyne, yeilding a total thrust of 1,500,000 pounds. The second stage identified as S-IV, was designed as a single cylinder with a common bulkhead separating the liquid oxygen from the liquid hydrogen. Propulsion was provided by six RL-10 engines built by Pratt Whitney, capable of producing a combined thrust of 90,000 pounds. Of the 10 Saturn I's planned, the first eight were designed and built at the Marshall Space Flight Center. The remaining two were built by the Chrysler Corporation

A graphic explaining the Tactical High-Mobility Terminal (THMT) image processing system. Country: Unknown

A graph depicting Soviet strategic surface-to-air missiles. Country: Unknown

This illustration depicts the Skylab-1 and Skylab-2 mission sequence. The goals of the Skylab were to enrich our scientific knowledge of the Earth, the Sun, the stars, and cosmic space; to study the effects of weightlessness on living organisms, including man; to study the effects of the processing and manufacturing of materials utilizing the absence of gravity; and to conduct Earth resource observations. The Skylab also conducted 19 selected experiments submitted by high school students. Skylab's 3 different 3-man crews spent up to 84 days in Earth orbit. The Marshall Space Flight Center (MSFC) had responsibility for developing and integrating most of the major components of the Skylab the Orbital Workshop (OWS), Airlock Module (AM), Multiple Docking Adapter (MDA), Apollo Telescope Mount (ATM), Payload Shroud (PS), and most of the experiments. MSFC was also responsible for providing the Saturn IB launch vehicles for three Apollo spacecraft and crews and a Saturn V launch vehicle for t

Maps and Charts - All States. Photographs Relating to National Forests, Resource Management Practices, Personnel, and Cultural and Economic History

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