Portal:Rocketry

Portal topics: Activities; Culture; Geography; Health; History; Mathematics; Nature; People; Philosophy; Religion; Society; Technology; Random portal

The Rocketry Portal

A rocket (from Italian: rocchetto, lit. 'bobbin/spool') is a vehicle that uses jet propulsion to accelerate without using any surrounding air. A rocket engine produces thrust by reaction to exhaust expelled at high speed. Rocket engines work entirely from propellant carried within the vehicle; therefore a rocket can fly in the vacuum of space. Rockets work more efficiently in a vacuum and incur a loss of thrust due to the opposing pressure of the atmosphere.

Multistage rockets are capable of attaining escape velocity from Earth and therefore can achieve unlimited maximum altitude. Compared with airbreathing engines, rockets are lightweight and powerful and capable of generating large accelerations. To control their flight, rockets rely on momentum, airfoils, auxiliary reaction engines, gimballed thrust, momentum wheels, deflection of the exhaust stream, propellant flow, spin, or gravity.

Rockets for military and recreational uses date back to at least 13th-century China. Significant scientific, interplanetary and industrial use did not occur until the 20th century, when rocketry was the enabling technology for the Space Age, including setting foot on the Moon. Rockets are now used for fireworks, missiles and other weaponry, ejection seats, launch vehicles for artificial satellites, human spaceflight, and space exploration.

Chemical rockets are the most common type of high power rocket, typically creating a high speed exhaust by the combustion of fuel with an oxidizer. The stored propellant can be a simple pressurized gas or a single liquid fuel that disassociates in the presence of a catalyst (monopropellant), two liquids that spontaneously react on contact (hypergolic propellants), two liquids that must be ignited to react (like kerosene (RP1) and liquid oxygen, used in most liquid-propellant rockets), a solid combination of fuel with oxidizer (solid fuel), or solid fuel with liquid or gaseous oxidizer (hybrid propellant system). Chemical rockets store a large amount of energy in an easily released form, and can be very dangerous. However, careful design, testing, construction and use minimizes risks. (Full article...)

Refresh with new selections below (purge)

Selected article - show another

NERVA XE in ETS-1

The Nuclear Engine for Rocket Vehicle Application (NERVA; /ˈnɜːrvə/) was a nuclear thermal rocket engine development program that ran for roughly two decades. Its principal objective was to "establish a technology base for nuclear rocket engine systems to be utilized in the design and development of propulsion systems for space mission application". It was a joint effort of the Atomic Energy Commission (AEC) and the National Aeronautics and Space Administration (NASA), and was managed by the Space Nuclear Propulsion Office (SNPO) until the program ended in January 1973. SNPO was led by NASA's Harold Finger and AEC's Milton Klein.

NERVA had its origins in Project Rover, an AEC research project at the Los Alamos Scientific Laboratory (LASL) with the initial aim of providing a nuclear-powered upper stage for the United States Air Force intercontinental ballistic missiles. Nuclear thermal rocket engines promised to be more efficient than chemical ones. After the formation of NASA in 1958, Project Rover was continued as a civilian project and was reoriented to producing a nuclear powered upper stage for NASA's Saturn V Moon rocket. Reactors were tested at very low power before being shipped to Jackass Flats in the Nevada Test Site. While LASL concentrated on reactor development, NASA built and tested complete rocket engines. (Full article...)

List of selected articles

edit

In the news

22 May 2024 –: Russia launches a Soyuz-2 rocket carrying the Kosmos 2576 satellite from the Plesetsk Cosmodrome launch site in Arkhangelsk Oblast. The United States Space Command accuses it of being an anti-satellite weapon capable of attacking other satellites, and is in the same orbit as a satellite operated by the National Reconnaissance Office. (Al Jazeera)
19 May 2024 – Russian invasion of Ukraine: At least six people are killed and 27 others are injured in a Russian double tap missile strike on a recreation area near Kharkiv. Separately, five people are killed and nine others are injured in a Russian strike using a multiple launch rocket system on two villages in Kupiansk Raion, Kharkiv Oblast. (Reuters)

Current events on Wikinews

edit

Topics

General images - load new batch

The following are images from various rocketry-related articles on Wikipedia.

Image 1Layout of a V-2 rocket. (from History of rockets)
Image 2The 'convocation of eagles chasing hare' rocket launcher from the Wubei Zhi (17th century). A double-ended rocket pod that carries 30 small poisoned rockets on each end for a total of 60 rockets. It carries a sling for transport. (from History of rockets)
Image 3RS-68 being tested at NASA's Stennis Space Center (from Rocket engine)
Image 4Opel RAK.1 - World's first public manned flight of a rocket plane on September 30, 1929. (from History of rockets)
Image 5A battery of Katyusha launchers fires at German forces during the Battle of Stalingrad, 6 October 1942 (from History of rockets)
Image 6Simplified diagram of a solid-fuel rocket:
1. Solid fuel–oxidiser mixture (propellant) packed into casing
2. Igniter initiates propellant combustion.
3. Central hole in propellant acts as the combustion chamber.
4. Exhaust nozzle expands and accelerates the gas jet to produce thrust.
5. Exhaust exits nozzle.
(from Rocket engine)
Image 7Typical ballistic missile sequence:
- 1. Launches by firing motor1(A)
- 2. Stage1 drops, motor2(B) ignites & shroud(E) ejects
- 3. Motor3(C) ignites and separates
- 4. Stage3 terminates and post-boost vehicle(D) separates
- 5. Vehicle maneuvers itself and prepares re-entry vehicle (RV)
- 6. RV with decoys and chaffs deploys
- 7. RV re-enters the atmosphere
- 8. Warhead(s) detonate on target
(from Missile)
Image 8Robert Esnault-Pelterie (1909). (from History of rockets)
Image 9Simplified diagram of a liquid-fuel rocket:
1. Liquid fuel tank
2. Liquid oxidiser tank
3. Pumps feed fuel and oxidiser under high pressure.
4. Combustion chamber mixes and burns the propellants.
5. Exhaust nozzle expands and accelerates the gas jet to produce thrust.
6. Exhaust exits nozzle.
(from Rocket engine)
Image 10Rocket carts from the Wubei Zhi (17th century) (from History of rockets)
Image 11The four expansion regimes of a de Laval nozzle:• under-expanded• perfectly expanded• over-expanded• grossly over-expanded (from Rocket engine)
Image 12Viking 5C rocket engine used on Ariane 1 through Ariane 4 (from Rocket engine)
Image 13A Tomahawk cruise missile in flight (from Missile)
Image 14Robert Anderson suggests using metal for rocket casing (from History of rockets)
Image 15Robert Goddard and the first liquid-fueled rocket. (from History of rockets)
Image 16An illustration of fire arrow launchers as depicted in the Wubei Zhi (17th century). The launcher is constructed using basketry. (from History of rockets)
Image 17A semi-active missile homing system (from Missile)
Image 18A "long serpent enemy breaking" fire arrow launcher as depicted in the Wubei Zhi (17th century). It carries 32 medium small poisoned rockets and comes with a sling to carry on the back. (from History of rockets)
Image 19Von Braun's rocket team in 1961 (from History of rockets)
Image 20Robert Goddard (from History of rockets)
Image 21French Diamant rocket, the second French rocket program, developed from 1961 (from History of rockets)
Image 22Rocket vehicle mechanical efficiency as a function of vehicle instantaneous speed divided by effective exhaust speed. These percentages need to be multiplied by internal engine efficiency to get overall efficiency. (from Rocket engine)
Image 23Armadillo Aerospace's quad vehicle showing visible banding (shock diamonds) in the exhaust jet (from Rocket engine)
Image 24The Congreve rocket (from History of rockets)
Image 25A simplified diagram of a solid-fuel rocket.
1. A propellant is packed with a hole in the middle
2. An igniter combusts the propellant
3. The hole acts as a combustion chamber
4. The hot exhaust is choked at the throat
5. Exhaust exits the rocket
(from Missile)
Image 26Rocket thrust is caused by pressures acting in the combustion chamber and nozzle. From Newton's third law, equal and opposite pressures act on the exhaust, and this accelerates it to high speeds. (from Rocket engine)
Image 27A V-1 flying bomb, amongst the first guided missiles (from Missile)
Image 28A German V-2 rocket on a Meillerwagen. (from History of rockets)