Aerobee 150

22.A booster lifts Aerobee 150 out of its launch rail.

The half-ton Aerobee could carry a 45.4-kilogram (100-pound) payload to an altitude of 120.6 kilometers (75 miles). For many years, the Aerobee was the standard American sounding rocket due to its reliability and relatively low cost. Several versions of the original Aerobee were produced. The Aerobee relied on a short-duration, solid-fuel booster for launching, after which the main-stage, liquid-propellant engine ignited.

On display at the NASM is an Aerobee 150, a more sophisticated version of the rocket. An Aerobee 150 can lift a 68.1-kilogram (150-pound) payload to an altitude of 274 kilometers (170 miles). Payloads consisted of a variety of scientific experiments.

The Aerobee concept originated early in 1946 when Dr. James Van Allen, then of the Applied Physics Laboratory at Johns Hopkins University, suggested that the Office of Naval Research contract for a rocket with these particular capabilities. The Aerojet General Corporation (then Aerojet, Inc.) was awarded the contract, with the Douglas Aircraft Corporation subcontracting for aerodynamic studies on the nose, fins, and tail cone, and for the final assembly of the rocket.

The Aerobee 150 is from the National Aeronautics and Space Administration, Goddard Space Flight Center.

23.Artist’s rendering of four-stage Farside sounding rocket, in launcher below balloon.

24.Rocket was fired directly through the apex of the balloon. Drawing shows the first stage falling away as second-stage rocket takes over.

Farside was a four-stage rocket launched from a balloon as an extremely high-altitude research vehicle. Achieving heights estimated at 6400 kilometers (4000 miles). Farside’s instrument payload was intended to study cosmic rays, earth’s magnetic field, certain forms of electromagnetic radiation in space, the presence of interplanetary gases, and the nature of meteoric dust.

The 908-kilogram (2000-pound) Farside was lifted to an altitude of 30.5 kilometers (19 miles) by a polyethylene balloon. An aluminum structure suspended from the balloon carried the 7.3-meter (24-foot) rocket to launch altitude. Positioned vertically in its casing, Farside was fired directly through the balloon.

Six Farsides were launched by the United States in 1957 from Eniwetok Atoll in the Pacific.

Farside’s first stage consisted of four solid-fuel Recruit rockets, manufactured by Thiokol Chemical Company. A single Recruit served as the second stage. Four Arrow II solid-fuel rockets by the Grand Central Rocket Company constituted the third stage. The final stage, a single Arrow II, carried the instrument payload provided by S. F. Singer of the University of Maryland.

Farside was developed by Aeronutronics Systems, Inc., for the U.S. Air Force Office of Scientific Research and Development.

The rocket on exhibit is from the Aeronutronics Division, Ford Motor Company.

25.Nike-Cajun ready for launch.

26.Nike-Cajun launch.

The Nike-Cajun was used extensively during International Geophysical Year (1957-58) to perform a variety of research tasks. These included weather photography, studies of water-vapor distribution in the upper atmosphere, and magnetic soundings in the ionosphere.

For photographic studies, the instrument package separated from the nose cone at about 80 kilometers (50 miles) and then coasted to a peak altitude of about 120 kilometers (75 miles), during which time data was collected. Then parachutes opened, lowering the cameras for recovery. Other data was radioed to Earth.

The Cajun rocket was developed by the Pilotless Aircraft Division of the National Advisory Committee for Aeronautics and the University of Michigan. The solid-fuel engine was designed and manufactured by Thiokol Chemical Company. The Nike booster was also solid fuel.

The rocket on exhibit is from the National Aeronautics and Space Administration.

27.Loading ARCAS into launcher.

All-purpose Rocket for Collecting Atmospheric Sounding (ARCAS) gathers local meteorological data helpful to weather forecasters. Its 5.4-kilogram (12-pound) payload may include instruments which measure temperature, pressure, humidity, wind velocity and direction, and magnetic conditions. The single-stage ARCAS vehicle reaches an altitude of 64 kilometers (40 miles), propelled by a slow-burning solid-fuel engine which produces 141.4 kilograms (312 pounds) of thrust.

When the ARCAS is boosted by a Sparrow or Sidewinder missile engine, it can reach altitudes of 182,880 meters (600,000 feet).

The 32-kilogram (71-pound) ARCAS is far less expensive than the larger two-stage weather rockets it has replaced. It was developed and produced by the Atlantic Research Corporation.

The ARCAS is from the Atlantic Research Corporation.

28.Preparing Cricket for launch.

The reusable Cricket, often called the “meteorologist’s handyman,” weighs only 2.5 kilograms (5½ pounds), 1.4 kilograms (3 pounds) of which is propellant. Recovered by parachute after each flight, Cricket costs less than $10 to refuel.

The Cricket’s .34-kilogram (three-fourth pound) instrument package zooms to 975 meters (3200 feet) in only 12 seconds, gathering data on air temperature, pressure and wind direction.

One of the rocket’s most noteworthy features is that it uses “cold” propellants. Compressed carbon dioxide to which acetone is added is pumped into a storage tank in the rocket at a pressure of 56.3 kilograms per square centimeter (800 pounds per square inch). Release of the pressurized mixture gives Cricket its thrust. Cricket is fired from its launcher by a separate charge of carbon dioxide in order to preserve the rocket’s fuel for flight.

This rocket was developed by Texaco Experiment, Inc., for the U.S. Air Force’s Cambridge Research Laboratory.

The Cricket is from Texaco, Inc.

29.Viking 12 lift-off.

The Viking rocket family, numbering 14, grew out of the Navy’s efforts to develop an upper atmosphere research program. With enough time between launches to incorporate modifications suggested by experience with earlier Vikings, no two rockets of the series were exactly alike; however, there were two basic types of Vikings. The first seven rockets were taller, thinner, and had larger fins than those numbered 8-14; rockets in the second set were heavier, with fuel capacity greatly increased, and were designed either to go higher than the early Vikings or to carry heavier payloads to the same altitude.

Viking’s highest altitude was 254 kilometers (158 miles) following a launch from White Sands on May 24, 1954. Experiments flown on these rockets measured air temperature, density, pressure, and composition, as well as providing cosmic and solar radiation data.

One of the few failures in this program was Viking 8, the first rocket of the second set, which unexpectedly tore loose from the launch stand while being test-fired.

Viking was conceived at the Naval Research Laboratory, designed and produced by the Glenn L. Martin Company of Baltimore, Maryland, and powered by a liquid-propellant engine by Reaction Motors, Inc.

The rocket on exhibit is from the Hayden Planetarium and Martin Marietta Aerospace.

30.MOUSE model displays some of the earliest solar cells made (under square cover on front).

The concept of artificial earth satellites was a logical extension of existing sounding-rocket programs. The MOUSE, or Minimum Orbital Unmanned Satellite of Earth, was conceived in 1951 as the smallest possible orbital vehicle capable of performing scientific tasks. While the MOUSE was never built or flown, it demonstrated what could be accomplished by an orbiting vehicle of modest size and weight.

The MOUSE would have weighed 45.4 kilograms (100 pounds). It was designed to study cosmic rays, interplanetary dust, and solar ultraviolet and X rays, with the instruments attached to rods projecting from either end. The satellite was to be powered by solar cells.

MOUSE was conceived by Kenneth W. Gatland, Anthony Kunesch, and Alan Dixon of England. Dr. S. F. Singer of the University of Maryland designed the MOUSE and constructed the model on exhibit. The model displays some of the earliest solar cells produced by the Bell Telephone Laboratories.

The MOUSE is from S. F. Singer.

31.Thor-Agena launch vehicle and its satellite payload before launch.

The Agena launch vehicle has been an integral part of both unmanned and manned space programs. Flown as an upper stage on Thor and Atlas boosters, Agena orbited an impressive roster of spacecraft including the Echo communications satellites, the Ranger and Lunar Orbiter Moon probes, and the Mariner vehicles that traveled to Venus and Mars.

As the target for docking experiments during Project Gemini, Agena made substantial contributions to the eventual success of the Apollo program. The vehicle earned the distinction of being the first to place a payload in polar orbit, and was also the first to achieve circular orbit. The Agena engine was the first which could be stopped and restarted in space.

The Agena launch vehicle was developed and manufactured by the Lockheed Missiles and Space Company for the United States Air Force.

The Agena-B is from the United States Air Force and the Lockheed Missile and Space Company.

32.The Agena Target Docking Vehicle seen from theGemini 8spacecraft during rendezvous approach.

33.Vanguard 1, second American satellite launched. Information fromVanguardshowed that the Earth is not quite round.

The first artificial earth satellites were sometimes called “long-playing rockets” because they carried the same instruments and investigated the same problems as had the sounding rockets. The great advantage of the satellite was its ability to provide a continuous flow of information for long periods of time. The first science satellites were the forerunners of later vehicles that would demonstrate the direct benefits that satellites could offer to such varied fields as weather observation and communication.

The advent of the earth satellite provided scientists with a new and valuable research tool. Science satellites have been used for such tasks as solar and astronomical observations, biology experiments, or atmospheric investigation. Explorer 1 (launched January 31, 1958) and Vanguard 1 (launched March 17, 1958), the first American earth satellites, carried scientific payloads into space.

Project Vanguard’s important contributions to America’s space program were the creation of the minitrack tracking system, the first use of silicon solar cells for electric power in a satellite, as well as the discovery that Earth is not quite round. The Vanguard program drew to a close with the 1959 launch of Vanguard 3. This satellite studied variations in solar and x-ray radiation and the earth’s magnetosphere. It also determined air density in the upper atmosphere.

The mysteries of the near-earth space environment drewExplorer 6, launched August 7, 1959.Explorer 6instruments measured radiation levels in the Van Allen radiation belts, mapped the earth’s magnetic field, counted micrometeorites, and studied the behavior of radio waves in space. In addition,Explorer 6carried a scanning device which returned the first complete television cloud-cover picture of the earth’s surface.

34.Artist’s concept of IMP-E. This satellite’s primary mission is to study solar wind and the interplanetary magnetic field at lunar distance and their interaction with the Moon.

Explorer 10, launched on board a Thor-Delta rocket on March 25, 1961, confirmed the existence of the solar wind—the stream of particles that carries the Sun’s magnetic field beyond the orbit of Earth. During the satellite’s planned 52 hours in orbit, it relayed information on the relationship between terrestrial and interplanetary magnetic fields and the solar wind.

To continue the study of solar wind and interplanetary magnetic fields,Explorer 12was orbited by a Delta launch vehicle on August 16, 1961. It was the first in a series of satellites to study energetic particles in space. These electrons and protons constitute the earth’s radiation belts and they affect weather and other phenomena on Earth.

Atmosphere Explorer-Awas the first of NASA’s aeronomy satellites. It was designed to remain in operation three months, studying the composition, density, pressure, and temperature of the upper atmosphere. This satellite discovered a belt of neutral helium atoms around the Earth.

Deriving its name from a spirit in Shakespeare’s play,The Tempest,Ariel 1explored the ionosphere, a region of electrically charged air which begins about 40 kilometers (25 miles) above the surface of the Earth. Launched April 26, 1962,Arielwas a cooperative venture between Great Britain and the United States. It was both the first British satellite and NASA’s first international satellite. The Royal Society’s British National Committee on Space Research coordinated the experimental program; NASA scientists and technicians built the craft.

Two small scientific laboratories, called Interplanetary Monitoring Platforms, were launched in 1967 to study the solar wind and other phenomena. IMP-E investigated interplanetary magnetic fields in the vicinity of the Moon. IMP-F investigated the interplanetary magnetic field also, in addition to the earth’s magnetosphere and radiation levels in space.

Interplanetary space between the Earth and Venus was the subject area forPioneer 5, launched March 11, 1960. The satellite tested long-range communications systems, developed methods for measuring astronomical distances, studied the effects of solar flares, and performed other tasks before it went into orbit around the Sun.

With increasing interest in the earth’s space environment, a satellite was launched on September 7, 1967, to investigate the impact of space on biological processes.Biosatellite 2was the second satellite in the program of three such vehicles. Frog eggs, plants, micro-organisms and insects were placed in orbit to enable scientists to study the combined effects of weightlessness, artificially produced radiation, and the absence of the normal day-night cycle on these organisms. Following two days in space, the capsule containing the experimental package reentered the atmosphere and was caught in mid-air by an Air Force recovery aircraft.

Vanguard 1is from John P. Hagan.Vanguard 3,Explorer 10,Explorer 12,AE-A,Ariel 1, IMP-E & F, andBiosatellite 2are from the National Aeronautics and Space Administration. The models ofExplorer 6andPioneer 5are from Space Technology Laboratories.

35.TOS satellite is covered with solar cells.

Weather forecasts are important to everyone—in planning whether or not to carry an umbrella, when to plant crops, when to evacuate riverbank areas. Nineteenth-century American meteorologists relied on local weather observations telegraphed to the Smithsonian Institution in Washington and then plotted on a large map of the nation from which forecasts were prepared.

WhenTiros-1returned the first global cloud-cover picture in 1960, meteorologists were on their way to more accurate forecasts. Since the satellite pictures offered more comprehensive weather data over a larger geographic area, the identification of weather patterns became more reliable.

While our knowledge of atmospheric conditions is still imperfect, we have learned to make reasonably accurate regional weather forecasts and to identify and track violent storms and hurricanes based on satellite information.

The TIROS series (Television Infrared Observations Satellites) were designed to test the feasibility of weather observation from orbit. The TIROS satellite on exhibit was the prototype for the entire series of vehicles. The prototype made eight trips to the launch stand at Cape Kennedy, where it was used to check communications and handling procedures prior to the launch of the scheduled TIROS. All 10 TIROS satellites were successful. Launched between April 1, 1960, and July 1, 1965, they carried a variety of camera systems for experimental purposes.

Nine TIROS Operational Satellites (TOS) followedTIROS 1-10. Except for the first TOS, these satellites flew in pairs with one craft storing pictures on board forlater transmission to major receiving centers, while the other broadcast its photographs continuously to any ground station within range. The satellite on display is of the latter type. These vehicles were launched between 1966 and 1969. They were placed in near-polar orbits by reliable Thor-Delta launch vehicles.

36.TIROS Iphoto showing a section of the East coast of the United States, including the Boston and New England area.

After launch, TOS vehicles were referred to as ESSA satellites. ESSA was an acronym both for Environmental Survey Satellite and for the Environmental Science Service Administration, the federal agency that operated the spacecraft. This organization became a part of the National Oceanic and Atmospheric Administration which currently has responsibility for operational meteorological satellite programs.

From about 1392 kilometers (865 miles) above Earth, two wide-angle television cameras mounted on either side of the spacecraft took in 10.4-million square kilometers (4-million square miles) per photo.

The Improved TIROS Operational Satellite (ITOS) opened the world of radiometric measurement to meteorologists—information about surface temperatures on the ground, at sea level, or at the cloud tops obtained by scanning devices sensitive to energy that is invisible to the naked eye. ITOS spacecraft could return accurate day or night surface and cloud-cover images. Seven of these satellites were launched between 1970 and 1973.

TIROSwas presented to the National Air and Space Museum by the National Aeronautics and Space Administration;TOSis from the National Oceanic and Atmospheric Administration;ITOSis from the Astro-Electronics Division of RCA, Inc.

37.Artist’s concept of ITOS weather satellite illustrating how the weather eye takes night-time (infrared) cloud-cover pictures.

38.Ground inflation test onEcho 1, the world’s first passive communications satellite.

Communications satellites can be grouped into two broad categories. Passive vehicles reflect signals from one ground station to another. Active satellites accept ground signals and either amplify and rebroadcast them immediately or record messages for later transmission.

The Echo satellite balloons typified the passive category of communications spacecraft. These satellites “bounced” radio signals from one ground station to another. Uninflated Echo payloads were carried into orbit packed in special storage containers. When released in space, the balloon was inflated by chemicals packed inside which subliminated to produce inflating gas. The mylar plastic skin of the satellite was sandwiched between two layers of aluminum foil.Echo 2—on display—included a system for releasing gas over a long period of time to maintain the satellite’s spherical shape. Launched January 25, 1964,Echo 2was thefirst satellite used for communication experiments between the United States and the Soviet Union.

Project West Ford, launched May 9, 1963, was a unique experiment in passive satellite communications. It was not a solid vehicle, but a series of 400-million tiny individual copper filaments called dipoles. The dipoles formed a reflective layer some 64,300 kilometers (40,000 miles) long, 32 kilometers (20 miles) thick, and 32 kilometers (20 miles) wide. The distance between the individual dipoles averaged 536 meters (one-third mile). The West Ford experiment proved disappointing, and advances in the design of active communications satellites made further experiments of this nature unnecessary.

Oscar 1(Orbital Satellite Carrying Amateur Radio) was conceived, designed, and constructed by American amateur radio “hams.” Launched as a “piggyback” satellite on December 12, 1963, Oscar transmitted a series of Morse code dots spelling “hi.” The message was picked up by 5000 operators in 28 nations during the 18 days of transmission. Oscar investigated radio propagation phenomena in space on that portion of the radio frequency spectrum allocated to amateur radio (144-146 megaherz).

Testing the use of a “delayed-repeater” satellite in global military communications,Courier 1-Bwas placed in a high-altitude orbit on October 4, 1960. The craft accepted and stored messages as it passed over one ground station, then replayed them on command.

Relay, another active repeater satellite, was placed in orbit on December 13, 1962.Relaycarried communications experiments to test a variety of relay equipment—including that for photofacsimile, teleprinter, and data transmission. During its 25-month lifespan,Relay 1introduced the nations of the world to satellite communication. A second, improvedRelaywas launched in 1964.

39.The exterior of eight-sidedRelayis composed of honeycomb aluminum panels studded with 8215 solar cells.

The world’s first commercial communications satellite was called “Early Bird,” or INTELSAT 1. Built a decade ago by Hughes Aircraft Company for Communications Satellite Corporation (COMSAT), Early Bird could transmit simultaneously on 240 two-way channels for telephone, telegraph, or data transmission. Transatlantic telephone circuit capability increased by 50 percent once Early Bird went into orbit on April 6, 1965. Although the craft had a life expectancy of 18 months, it operated satisfactorily in full-time service for more than three and one-half years.

INTELSAT 2 introduced multipoint communications between earth stations in the Northern and Southern hemispheres. With almost twice the power of Early Bird, INTELSAT 2 proved particularly important as communications support for the Apollo missions to the Moon.

INTELSAT 2 established a global network of three satellites that was effective in linking two-thirds of the world’s people in one communications chain. The first of the series was launched on January 11, 1967. These spacecraft were designed and manufactured by the Hughes Aircraft Company for Intelsat, Inc., and had a design lifetime of three years.

INTELSAT 3 was a series of five communications satellites which provided global coverage for the first time. This INTELSAT had a capacity of 2400 voice, data, facsimile, and telegraph circuits, plus four television channels and had a design lifetime of five years.

The satellite featured a de-spun antenna which remained pointed at a particular area of the globe, while the body of the satellite spun around it. It was the first commercial satellite capable of transmitting voice and television broadcasts simultaneously.

INTELSAT 3 satellites were manufactured by TRW Systems, Inc., for Intelsat, Inc.

Echo 2,Courier 1-B, andRelayare from the National Aeronautics and Space Administration;OSCAR 1is from Project Oscar, Inc.; INTELSAT 1, INTELSAT 2, and INTELSAT 3 are from the International Telecommunications Satellite Organization.

40.Apollo 15 Lunar Module, center, on the Moon. Astronaut Irwin on left and Lunar Roving Vehicle on right.

The lunar module is one of twelve built for the Apollo moon-landing program. Although this one never flew because an earlier test flight was completely successful, two-stage lunar modules like this one have been used for each manned moon landing.

Lunar modules do not have to be streamlined for flights through the vacuum of space or to withstand reentry. The lunar module (LM) lifts off from Earth enclosed in a compartment of the Saturn 5 launch vehicle, below the command-service module that houses the astronauts. The command module pulls the LM from its storage area once the spacecraft are on their way to the Moon, and the two travel together until they arrive in lunar orbit.

When the crew is ready to land, two of the three astronauts enter the LM and undock it, leaving the third to pilot the command module. After touchdown on the Moon, the astronauts exit through the door above the ladder.

The silver and black ascent stage, containing the astronauts’ pressurized compartment and the clusters of rockets that control the spacecraft, fits on top of the shiny gold descent stage that actually touches down on the Moon. The descent stage contains a main, centrally located rocket engine. This segment of the craft remains on the Moon as the crew lifts off in the ascent stage to rejoin the command module.

After the crew transfers to the command module, the ascent stage is also left behind as the three crew members start their return journey.

The LM is displayed just as it would look during a moon-landing mission. The gold and black materials insulate the spacecraft’s inner structure from temperature extremes and protect it from micrometeoroids. Thin sheets of both materials are used in “blankets” to accomplish the necessary protection in a foreign environment.

The black material is heat-resistant nickel-steel alloy. Each sheet is only .002 millimeters (1/12,000 of an inch) thick. These absorb heat and radiate it back into the blackness of space.

The shiny gold material on the descent stage is aluminum that is thinly coated over plastic film. The thin sheets of plastic and aluminum are used in blankets of up to 25 layers for protection and insulation of the spacecraft.

Prime contractor for the lunar module was Grumman Aerospace Corporation.

The lunar module on exhibit is from the National Aeronautics and Space Administration.

41.Lunar Module Center Instrument Panel in the ascent stage.

42.Lunar Orbiter.

The Lunar Orbiter project was initiated in 1963 as part of the U.S. Apollo program to land men on the Moon during the decade of the nineteen sixties.

Lunar Orbiter’s primary mission was to take and transmit both wide-angle and closeup images of the Moon. Lunar Orbiters photographed many areas of scientific interest and provided general photographic coverage of much of the moon’s surface. These pictures were then used to select the best landing sites for the first manned lunar landings. Orbiters also showed that the moon’s gravitational field permitted stable orbits.

Lunar Orbiter 1was launched atop an Atlas-Agena D rocket on August 10, 1966. The last in the project,Lunar Orbiter 5, was launched on August 1, 1967. All five missions were successful.

The first three missions were similar. After each launch, the Agena stage’s booster engine was fired to send the spacecraft on a 90-hour coasting trajectory to the Moon, about 386,160 kilometers (240,000 miles) distant.

As the spacecraft neared the Moon, its on-board engine was fired as a retrorocket to slow theOrbiterand permit it to go into orbit around the Moon.

The closest approach to the Moon in each orbit was about 45 kilometers (28 miles), and the spacecraft swung out to about 1850 kilometers (1150 miles) from the Moon.

Photography was conducted while theOrbiterwas near the lunar surface. Lunar photography for the Apollo Program landing-site selection was completed by the first three Lunar Orbiters. Each was then intentionally crashed into the Moon to prevent it from interfering with later missions.

The last two Lunar Orbiters were used for scientific photography of the Moon. Both were placed into polar orbits so that they could photograph all of the sunlit areas of the Moon.

Each Lunar Orbiter carried a camera with both a telephoto and a wide-angle lens. The telephoto lens was capable of resolving objects on the lunar surface as small as 91.4 centimeters (three feet) in diameter. The wide-angle lens could resolve objects as small as 7.6 meters (25 feet) in diameter. The photographic images were converted to electrical signals for transmission to Earth.

The Lunar Orbiter project was a complete success. All spacecraft operated properly, photographing a total of more than 36-million square kilometers (14-million square miles) of the moon’s surface.

Prime contractor for the Lunar Orbiter program was the Boeing Company. Principal subcontractors were Eastman Kodak Company and RCA.

The Lunar Orbiter in the National Air and Space Museum’s collection was used for thermal testing of spacecraft systems.

Lunar Orbiteris from the National Aeronautics and Space Administration.

43.Surveyor.

44.Apollo 12crewman examinesSurveyor 3, which soft-landed on the Moon on April 19, 1967. TheApollo 12(1969) Lunar Module is in the background.

The Surveyor Project, begun in 1960, consisted of seven unmanned spacecraft which were launched between May 30, 1966, and January 6, 1968. The craft were used to develop lunar soft-landing techniques, to survey potential Apollo landing sites, and to improve scientific understanding of the Moon.

Five of the seven Surveyor spacecraft successfully landed on the Moon and performed their tasks well. They responded to 600,545 commands from Earth and returned 87,632 television images of their lunar surroundings. (Surveyors 2and4crashed into the Moon and were destroyed.)

Besides returning TV images,Surveyors 3,5,6, and7carried a soil-sampling claw which could dig a trench, and test soil hardness and other characteristics. The soil-sampler tests showed that the lunar surface would bear the weight of an Apollo Lunar Module.

Surveyors 5,6, and7carried instruments capable of making simple chemical analyses of the lunar soil near the spacecraft. This information told scientists that most lunar soil near the Surveyors was basalt, a common rock on Earth as well.

The Surveyor spacecraft on exhibit, designatedS-10, was used in ground-based tests of on-board equipment, and was not used on a mission.S-10is exhibited as it would have appeared just before landing on the Moon.

Prime contractor for the Surveyor spacecraft was the Hughes Aircraft Company. The project was managed by the National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California.

The spacecraft on exhibit is from the National Aeronautics and Space Administration.

The American pioneer of astronautics, Robert H. Goddard (1882-1945) not only outlined the physical principles that would govern space flight, but he also constructed and tested many rocket engines, airframes, control devices, and guidance mechanisms between 1926 and 1942.

Goddard held a doctorate in physics, and was a professor at Clark University, Worcester, Massachusetts. The Smithsonian Institution began funding Goddard’s experiments as early as 1917 and published his first major work,A Method of Reaching Extreme Altitudes, in 1919.

Goddard was not only a trained scientist, but a talented and ingenious engineer as well. On March 16, 1926, he launched the world’s first liquid-propellant rocket. By 1930, he had established a rocket test facility at Mescalero Ranch, near Roswell, New Mexico. Here, he conducted research, funded by the Daniel and Florence Guggenheim Foundation, on rocket power plants, pumps and fuel systems, control mechanisms, and other vital elements of the modern rocket.

This vehicle is the oldest surviving liquid-propellant rocket in the world. Built of parts employed in the first liquid-propellant rocket launched on March 16, 1926, the engine was moved from the nose of the vehicle to the rear for the May 4 trial. Other changes were introduced to reduce the weight of the rocket to 2.5 kilograms (5.5 pounds). The motor burned gasoline and liquid oxygen.

The alcohol burner under the liquid oxygen tank was inadvertently not ignited, causing the May 4 attempted launch to fail. A second test on May 5 also proved unsuccessful. However, the rocket engine was fired on both occasions.

The May 4 rocket is from Mrs. Robert H. Goddard and the Daniel and Florence Guggenheim Foundation.

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