55 relations: AJ10, Angle of attack, Apollo 14, Apollo 15, Apollo 16, Apollo 17, Apollo 5, Apollo 7, Apollo abort modes, Apollo Command/Service Module, Apollo Lunar Module, Apollo Lunar Surface Experiments Package, Apollo PGNCS, Apollo program, Apollo–Soyuz Test Project, Ascent Propulsion System, Attitude control, Boilerplate (spaceflight), Canard (aeronautics), Descent Propulsion System, Detonating cord, Directional antenna, Dynamic pressure, Earth, Fuel cell, Grumman, Heat shield, Hypergolic propellant, Launch escape system, Launch vehicle, Little Joe II, Lockheed Propulsion Company, Lunar orbit rendezvous, Lunar rover, Moon, Pad Abort Test 1, Pad Abort Test 2, Parachute, Pitot tube, Reaction control system, Redundancy (engineering), Rockwell International, S-IVB, Saturn (rocket family), Saturn IB, Saturn V, Saturn V Instrument Unit, Skylab, Solid-propellant rocket, Space rendezvous, ..., Spacecraft, Thiokol, Thrust, Translation (geometry), Truss. Expand index (5 more) » « Shrink index
The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet).
In fluid dynamics, angle of attack (AOA, or \alpha (Greek letter alpha)) is the angle between a reference line on a body (often the chord line of an airfoil) and the vector representing the relative motion between the body and the fluid through which it is moving.
Apollo 14 was the eighth manned mission in the United States Apollo program, and the third to land on the Moon.
Apollo 15 was the ninth manned mission in the United States' Apollo program, the fourth to land on the Moon, and the eighth successful manned mission.
Apollo 16 was the tenth manned mission in the United States Apollo space program, the fifth and penultimate to land on the Moon and the first to land in the lunar highlands.
Apollo 17 was the final mission of NASA's Apollo program.
Apollo 5 (also known as AS-204), was the first unmanned flight of the Apollo Lunar Module (LM), which would later carry astronauts to the lunar surface.
Apollo 7 was an October 1968 human spaceflight mission carried out by the United States.
During the launch of an Apollo spacecraft by the Saturn IB or Saturn V rocket, the flight could be aborted to rescue the crew if the rocket failed catastrophically.
The Command/Service Module (CSM) was one of the two United States '''Apollo''' spacecraft, used for the Apollo program which landed astronauts on the Moon between 1969 and 1972.
The Lunar Module (LM, pronounced "Lem"), originally designated the Lunar Excursion Module (LEM), was the lander portion of the Apollo spacecraft built for the US Apollo program by Grumman Aircraft to carry a crew of two from lunar orbit to the surface and back.
The Apollo Lunar Surface Experiments Package (ALSEP) comprised a set of scientific instruments placed by the astronauts at the landing site of each of the five Apollo missions to land on the Moon following Apollo 11 (Apollos 12, 14, 15, 16, and 17).
The Apollo Primary Guidance, Navigation and Control System (PGNCS) (pronounced pings) was a self-contained inertial guidance system that allowed Apollo spacecraft to carry out their missions when communications with Earth were interrupted, either as expected, when the spacecraft were behind the Moon, or in case of a communications failure.
The Apollo program, also known as Project Apollo, was the third United States human spaceflight program carried out by the National Aeronautics and Space Administration (NASA), which accomplished landing the first humans on the Moon from 1969 to 1972.
The Apollo–Soyuz Test Project (ASTP) (Экспериментальный полёт «Аполлон» - «Союз» (ЭПАС), Eksperimentalniy polyot Apollon-Soyuz, lit. "Experimental flight Apollo-Soyuz", commonly referred to by the Soviets as "Soyuz-Apollo"), conducted in July 1975, was the first joint U.S.–Soviet space flight, as a symbol of the policy of détente that the two superpowers were pursuing at the time.
The Ascent Propulsion System (APS) or LMAE (Lunar Module Ascent Engine) is a fixed thrust hypergolic rocket engine developed by Bell Aerosystems for use in the Apollo Lunar Module Ascent Stage.
Attitude control is controlling the orientation of an object with respect to an inertial frame of reference or another entity like the celestial sphere, certain fields, and nearby objects, etc.
A boilerplate spacecraft, also known as a mass simulator, is a nonfunctional craft or payload that is used to test various configurations and basic size, load, and handling characteristics of rocket launch vehicles.
A canard is an aeronautical arrangement wherein a small forewing or foreplane is placed forward of the main wing of a fixed-wing aircraft.
The Descent Propulsion System (DPS) or LMDE (Lunar Module Descent Engine) is a variable throttle hypergolic rocket engine developed by Space Technology Laboratories (TRW) for use in the Apollo Lunar Module Descent Stage.
Detonating cord (also called detonation cord, detacord, det. cord, detcord, primer cord or sun cord) is a thin, flexible plastic tube usually filled with pentaerythritol tetranitrate (PETN, pentrite).
A directional antenna or beam antenna is an antenna which radiates or receives greater power in specific directions allowing increased performance and reduced interference from unwanted sources.
Dynamic pressure (sometimes called velocity pressure) is the increase in a moving fluid's pressure over its static value due to motion.
Earth is the third planet from the Sun and the only astronomical object known to harbor life.
A fuel cell is an electrochemical cell that converts the chemical energy from a fuel into electricity through an electrochemical reaction of hydrogen fuel with oxygen or another oxidizing agent.
The Grumman Aircraft Engineering Corporation, later Grumman Aerospace Corporation, was a leading 20th century U.S. producer of military and civilian aircraft.
A heat shield is designed to shield a substance from absorbing excessive heat from an outside source by either dissipating, reflecting or simply absorbing the heat.
A hypergolic propellant combination used in a rocket engine is one whose components spontaneously ignite when they come into contact with each other.
A launch escape system (LES) or launch abort system (LAS) is a crew safety system connected to a space capsule, used to quickly separate the capsule from its launch vehicle rocket in case of a launch abort emergency, such as an impending explosion.
A launch vehicle or carrier rocket is a rocket used to carry a payload from Earth's surface through outer space, either to another surface point (suborbital), or into space (Earth orbit or beyond).
Little Joe II was an American rocket used from 1963–66 for five unmanned tests of the Apollo spacecraft Launch Escape System (LES), and to verify the performance of the Command Module parachute recovery system in abort mode.
The Lockheed Propulsion Company was a division of the Lockheed Aircraft Corporation located at 1500 Crafton Avenue in the Mentone, California area northeast of Redlands, California, adjacent to the Santa Ana River, from 1961 to 1975.
Lunar orbit rendezvous (LOR) is a key concept for efficiently landing humans on the Moon and returning them to Earth.
A lunar rover or Moon rover is a space exploration vehicle (rover) designed to move across the surface of the Moon.
The Moon is an astronomical body that orbits planet Earth and is Earth's only permanent natural satellite.
Pad Abort Test 1 was the first abort test of the Apollo spacecraft on November 7, 1963.
Pad Abort Test 2 was the follow-on second abort test to Pad Abort Test 1 of the Apollo spacecraft.
A parachute is a device used to slow the motion of an object through an atmosphere by creating drag (or in the case of ram-air parachutes, aerodynamic lift).
A Pitot tube, also known as Pitot probe, is a flow measurement device used to measure fluid flow velocity.
A reaction control system (RCS) is a spacecraft system that uses thrusters to provide attitude control, and sometimes translation.
In engineering, redundancy is the duplication of critical components or functions of a system with the intention of increasing reliability of the system, usually in the form of a backup or fail-safe, or to improve actual system performance, such as in the case of GNSS receivers, or multi-threaded computer processing.
Rockwell International was a major American manufacturing conglomerate in the latter half of the 20th century, involved in aircraft, the space industry, both defense-oriented and commercial electronics, automotive and truck components, printing presses, valves and meters, and industrial automation.
The S-IVB (sometimes S-4B, always pronounced "ess four bee") was built by the Douglas Aircraft Company and served as the third stage on the Saturn V and second stage on the Saturn IB.
The Saturn family of American rocket boosters was developed by a team of mostly German rocket scientists led by Wernher von Braun to launch heavy payloads to Earth orbit and beyond.
The Saturn IB (pronounced "one B", also known as the Uprated Saturn I) was an American launch vehicle commissioned by the National Aeronautics and Space Administration (NASA) for the Apollo program.
The Saturn V (pronounced "Saturn five") was an American human-rated expendable rocket used by NASA between 1967 and 1973.
The Saturn V Instrument Unit is a ring-shaped structure fitted to the top of the Saturn V rocket's third stage (S-IVB) and the Saturn IB's second stage (also an S-IVB).
Skylab was the United States' space station that orbited the Earth from 1973 to 1979, when it fell back to Earth amid huge worldwide media attention.
A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer).
A space rendezvous is an orbital maneuver during which two spacecraft, one of which is often a space station, arrive at the same orbit and approach to a very close distance (e.g. within visual contact).
A spacecraft is a vehicle or machine designed to fly in outer space.
Thiokol (variously Thiokol Chemical Corporation, Morton-Thiokol Inc., Cordant Technologies Inc., Thiokol Propulsion, AIC Group, ATK Thiokol, ATK Launch Systems Group; finally Orbital ATK before becoming part of Northrop Grumman Innovation Systems) was an American corporation concerned initially with rubber and related chemicals, and later with rocket and missile propulsion systems.
Thrust is a reaction force described quantitatively by Newton's third law.
In Euclidean geometry, a translation is a geometric transformation that moves every point of a figure or a space by the same distance in a given direction.
In engineering, a truss is a structure that "consists of two-force members only, where the members are organized so that the assemblage as a whole behaves as a single object".