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PROPELLANT

  • Propellant
  • Chemical substance used for propulsion

    A propellant (or propellent) is a mass that is expelled or expanded in such a way as to create a thrust or another motive force in accordance with Newton's

    Propellant

    Propellant

  • Rocket propellant
  • Chemical or mixture used in a rocket engine

    Rocket propellant is used as a reaction mass ejected from a rocket engine to produce thrust. The energy required can either come from the propellants themselves

    Rocket propellant

    Rocket propellant

    Rocket_propellant

  • Solid-propellant rocket
  • Rocket with a motor that uses solid propellants

    A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel

    Solid-propellant rocket

    Solid-propellant rocket

    Solid-propellant_rocket

  • Hypergolic propellant
  • Type of rocket engine fuel

    hypergolic in Wiktionary, the free dictionary. A hypergolic propellant is a rocket propellant whose components spontaneously ignite upon contact with one

    Hypergolic propellant

    Hypergolic propellant

    Hypergolic_propellant

  • Liquid rocket propellant
  • Liquid form of rocket propellants

    The highest specific impulse chemical rockets use liquid propellants (liquid-propellant rockets). They can consist of a single chemical (a monopropellant)

    Liquid rocket propellant

    Liquid_rocket_propellant

  • Propellant 23
  • Topics referred to by the same term

    Propellant 23 may refer to: Fluoroform Propellant 23 (The Avengers) This disambiguation page lists articles associated with the title Propellant 23. If

    Propellant 23

    Propellant_23

  • Liquid-propellant rocket
  • Rocket engine that uses liquid fuels and oxidizers

    liquid-propellant rocket or liquid rocket uses a rocket engine burning liquid propellants. (Alternate approaches use gaseous or solid propellants.) Liquids

    Liquid-propellant rocket

    Liquid-propellant rocket

    Liquid-propellant_rocket

  • Smokeless powder
  • Type of firearm propellant

    Smokeless powder is a type of propellant used in firearms and artillery that produces less smoke and less fouling when fired compared to black powder.

    Smokeless powder

    Smokeless powder

    Smokeless_powder

  • Caseless ammunition
  • Type of weapon-cartridge

    cartridge case that typically holds the primer, propellant and projectile together as a unit. Instead, the propellant and primer are fitted to the projectile

    Caseless ammunition

    Caseless ammunition

    Caseless_ammunition

  • Orbital propellant depot
  • Cache of propellant used to refuel spacecraft

    An orbital propellant depot is a cache of propellant that is placed in orbit around Earth or another body to allow spacecraft or the transfer stage of

    Orbital propellant depot

    Orbital propellant depot

    Orbital_propellant_depot

  • Firearm propellant
  • Type of propellant

    Firearm propellants are a specialized type of propellant used to discharge a projectile (typically a bullet, slug, or pellets) through the barrel of a

    Firearm propellant

    Firearm propellant

    Firearm_propellant

  • Rocket engine
  • Non-airbreathing engine used to propel a missile or vehicle

    high-speed jet of high-temperature gas produced by the combustion of rocket propellant stored inside the rocket. Space vehicles carry their own oxidizer, unlike

    Rocket engine

    Rocket engine

    Rocket_engine

  • Ball propellant
  • Form of nitrocellulose used in small arms cartridges

    cartridges. Ball propellant can be manufactured more rapidly with greater safety and less expense than extruded propellants. Ball propellant was first used

    Ball propellant

    Ball propellant

    Ball_propellant

  • Rocket
  • Vehicle propelled by ejection of gases

    expelled at high speed. Unlike jet engines, rockets are fuelled entirely by propellant which they carry, without the need for oxygen from air; consequently a

    Rocket

    Rocket

    Rocket

  • Propellant tank
  • Type of container in a vehicle

    A propellant tank is a container which is part of a vehicle, where propellant is stored prior to use. Propellant tanks vary in construction, and may be

    Propellant tank

    Propellant_tank

  • Propellant management device
  • Device to expel propellant in low gravity

    A propellant management device (PMD) provides a way to expel propellant in a low-gravity environment. Devices can use surface tension as the primary expulsion

    Propellant management device

    Propellant_management_device

  • Starship Propellant Transfer Demonstration
  • First propellant transfer between Starships

    The SpaceX Starship Propellant Transfer Demo is a planned demonstration of essential capabilities required for refueling a Starship in low-Earth orbit

    Starship Propellant Transfer Demonstration

    Starship_Propellant_Transfer_Demonstration

  • ALICE (propellant)
  • Nano-aluminum powder rocket propellant

    Aluminum-Ice Rocket Propellant, or ALICE, is a rocket propellant that consists of a frozen mixture of nano-aluminum powder and water (i.e. aluminum and

    ALICE (propellant)

    ALICE_(propellant)

  • Specific impulse
  • Change in velocity per amount of fuel

    efficiently an engine, such as a rocket or jet engine, generates thrust from propellant. Isp is the effective exhaust velocity used in the Tsiolkovsky rocket

    Specific impulse

    Specific_impulse

  • Aerosol spray dispenser
  • Dispensing system of an aerosol mist

    particles. It comprises a can or bottle that contains a payload, and a propellant under pressure. When the container's valve is opened, the payload is forced

    Aerosol spray dispenser

    Aerosol spray dispenser

    Aerosol_spray_dispenser

  • Ammonium perchlorate composite propellant
  • Solid-rocket propellant

    perchlorate composite propellant (APCP) is a solid rocket propellant. It differs from many traditional solid rocket propellants such as black powder or

    Ammonium perchlorate composite propellant

    Ammonium_perchlorate_composite_propellant

  • Staged combustion cycle
  • Rocket engine operation method

    cycle of a bipropellant rocket engine. In the staged combustion cycle, propellant flows through multiple combustion chambers, and is thus combusted in stages

    Staged combustion cycle

    Staged combustion cycle

    Staged_combustion_cycle

  • Propellant mass fraction
  • Concept in aerospace engineering

    In aerospace engineering, the propellant mass fraction is the portion of a vehicle's mass which does not reach the destination, usually used as a measure

    Propellant mass fraction

    Propellant_mass_fraction

  • Cartridge (firearms)
  • Pre-assembled firearm ammunition

    firearm ammunition packaging a projectile (bullet, shot, or slug), a propellant substance (smokeless powder, black powder substitute, or black powder)

    Cartridge (firearms)

    Cartridge (firearms)

    Cartridge_(firearms)

  • Ion thruster
  • Form of electric spacecraft propulsion

    similar to a gridded electrostatic ion thruster and used mercury for propellant. Suborbital tests were conducted during the 1960s and in 1964, and the

    Ion thruster

    Ion thruster

    Ion_thruster

  • RP-1
  • Highly refined form of kerosene used as rocket fuel

    RP-1 (Rocket Propellant-1 or Refined Petroleum-1) and similar fuels like RG-1 and T-1 are highly refined kerosene formulations used as rocket fuel. Liquid-fueled

    RP-1

    RP-1

    RP-1

  • Heckler & Koch G11
  • Caseless ammunition assault rifle prototype

    Heckler & Koch (mechanical engineering and weapon design), Dynamit Nobel (propellant composition and projectile design), and Hensoldt Wetzlar (target identification

    Heckler & Koch G11

    Heckler & Koch G11

    Heckler_&_Koch_G11

  • Hybrid-propellant rocket
  • Rocket engine that uses both liquid / gaseous and solid fuel

    A hybrid-propellant rocket is a rocket with a rocket motor that uses rocket propellants in two different phases: one solid and the other either gas or

    Hybrid-propellant rocket

    Hybrid-propellant rocket

    Hybrid-propellant_rocket

  • JP-7
  • Jet fuel formulation for certain supersonic aircraft

    Fuel Low Volatility JP-7, commonly known as JP-7 (referred to as Jet Propellant 7 prior to MIL-DTL-38219) is a specialized type of jet fuel developed

    JP-7

    JP-7

    JP-7

  • SpaceX Starship
  • Reusable superheavy-lift general-purpose launch vehicle

    tank, the liquid methane tank, and the interstage. The two cryogenic propellant tanks on Super Heavy are separated by a common bulkhead, a similar structural

    SpaceX Starship

    SpaceX Starship

    SpaceX_Starship

  • Cordite
  • Smokeless propellant

    family of smokeless propellants developed and produced in Britain since 1889 to replace black powder as a military firearm propellant. Cordite is made by

    Cordite

    Cordite

    Cordite

  • Zero-propellant maneuver
  • A zero-propellant maneuver (ZPM) is an optimal attitude trajectory used to perform spacecraft rotational control without the need to use thrusters. ZPMs

    Zero-propellant maneuver

    Zero-propellant maneuver

    Zero-propellant_maneuver

  • Falcon Heavy
  • Partially reusable super-heavy-lift launch vehicle by SpaceX

    Green Propellant Infusion Mission (GPIM) was a payload; it is a project partly developed by the U.S. Air Force to demonstrate a less-toxic propellant. Another

    Falcon Heavy

    Falcon Heavy

    Falcon_Heavy

  • Ammunition
  • Material fired, scattered, dropped, or detonated from a weapon or weapon system

    single package. Until the 20th century, black powder was the most common propellant used, but it has now been replaced in nearly all cases by modern compounds

    Ammunition

    Ammunition

    Ammunition

  • Internal ballistics
  • Study of the propulsion of a projectile

    a projectile. In guns, internal ballistics covers the time from the propellant's ignition until the projectile exits the gun barrel. The study of internal

    Internal ballistics

    Internal_ballistics

  • Green Propellant Infusion Mission
  • NASA satellite testing a new rocket fuel

    The Green Propellant Infusion Mission (GPIM) was a NASA technology demonstrator project that tested a less toxic and higher performance/efficiency chemical

    Green Propellant Infusion Mission

    Green Propellant Infusion Mission

    Green_Propellant_Infusion_Mission

  • Starship flight 14
  • First operational flight of the SpaceX Starship

    after launch. After splashdown, Ship 41 tipped onto its side and residual propellant ignited. SpaceX had not planned to recover the spacecraft from the ocean

    Starship flight 14

    Starship_flight_14

  • Tsiolkovsky rocket equation
  • Mathematical equation describing the motion of a rocket

    initial total mass, including propellant, a.k.a. wet mass; m f {\displaystyle m_{f}} is the final total mass without propellant, a.k.a. dry mass. Given the

    Tsiolkovsky rocket equation

    Tsiolkovsky rocket equation

    Tsiolkovsky_rocket_equation

  • Gunpowder
  • Type of firearm propellant

    while the saltpeter is an oxidizer. Gunpowder has been widely used as a propellant in firearms, artillery, rocketry, and pyrotechnics, including use as a

    Gunpowder

    Gunpowder

    Gunpowder

  • 2026 Iran war
  • Ongoing armed conflict in West Asia

    launch vehicles, including the (Islamic Revolutionary Guard Corps') solid-propellant Ghaem-100, could clearly reach longer ranges than their regional missile

    2026 Iran war

    2026_Iran_war

  • Hydroxyl-terminated polybutadiene
  • Chemical compound

    Similar propellants, often referred to as APCP (ammonium perchlorate composite propellant) are used in larger model rockets. A typical APCP propellant mixture

    Hydroxyl-terminated polybutadiene

    Hydroxyl-terminated_polybutadiene

  • St. Marks Powder
  • Ammunition manufacturer in the United States of America

    of General Dynamics Ordnance and Tactical Systems manufacturing ball propellant in Crawfordville, Florida. St. Marks makes about 15,000[citation needed]

    St. Marks Powder

    St. Marks Powder

    St._Marks_Powder

  • Saturn V
  • American super heavy-lift expendable rocket

    000 kg (310,000 lb), which included the S-IVB third stage with remaining propellant to send the Apollo command and service module and Lunar Module to the

    Saturn V

    Saturn V

    Saturn_V

  • Autogenous pressurization
  • Use of self-generated gaseous propellant

    the use of self-generated gaseous propellant to pressurize liquid propellant in rockets. Traditional liquid-propellant rockets have been most often pressurized

    Autogenous pressurization

    Autogenous pressurization

    Autogenous_pressurization

  • Space Shuttle Solid Rocket Booster
  • Solid propellant rocket used by the Space Shuttle

    The Space Shuttle Solid Rocket Booster (SRB) was the first solid-propellant rocket to be used for primary propulsion on a vehicle used for human spaceflight

    Space Shuttle Solid Rocket Booster

    Space Shuttle Solid Rocket Booster

    Space_Shuttle_Solid_Rocket_Booster

  • Dichlorodifluoromethane
  • Chemical compound

    chlorofluorocarbon halomethane (CFC) used as a refrigerant and aerosol spray propellant. In compliance with the Montreal Protocol, its manufacture was banned

    Dichlorodifluoromethane

    Dichlorodifluoromethane

  • Rocket mass ratio
  • Measure of the efficiency of a rocket based on its propellant's mass

    massive the vehicle is with propellant than without. It is the ratio of the rocket's wet mass (vehicle plus contents plus propellant) to its dry mass (vehicle

    Rocket mass ratio

    Rocket_mass_ratio

  • Solid rocket booster
  • Solid propellant motor used to augment the thrust of a rocket

    A solid rocket booster (SRB) is a solid propellant motor used to provide thrust in spacecraft launches from initial launch through the first ascent. Many

    Solid rocket booster

    Solid rocket booster

    Solid_rocket_booster

  • Bulk loaded liquid propellants
  • Bulk-loaded liquid propellants (BLP) are an artillery technology that was pursued at the U.S. Army Research Laboratory and U.S. Naval Weapons Center from

    Bulk loaded liquid propellants

    Bulk_loaded_liquid_propellants

  • Recoilless rifle
  • Type of light artillery gun

    man-portable launcher that is designed to eject some form of countermass such as propellant gas from the rear of the weapon at the moment of firing, creating forward

    Recoilless rifle

    Recoilless rifle

    Recoilless_rifle

  • Electric-pump-fed engine
  • Rocket engine operation method

    which the fuel pumps are electrically powered, and so all of the input propellant is directly burned in the main combustion chamber, and none is diverted

    Electric-pump-fed engine

    Electric-pump-fed engine

    Electric-pump-fed_engine

  • Missile
  • Self-propelled guided weapon system

    airborne ranged weapon capable of self-propelled flight aided usually by a propellant, jet engine or rocket engine. Historically, 'missile' referred to any

    Missile

    Missile

    Missile

  • Rocket candy
  • Sugar-based rocket propellant

    is a type of rocket propellant for model rockets made with a form of sugar as a fuel, and containing an oxidizer. The propellant can be divided into three

    Rocket candy

    Rocket candy

    Rocket_candy

  • Pressure-fed engine
  • Rocket engine operation method

    engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and oxidizer to the combustion chamber. To maintain

    Pressure-fed engine

    Pressure-fed engine

    Pressure-fed_engine

  • Hydroxylammonium nitrate
  • Chemical compound

    used as a rocket propellant either as a solution in monopropellants or bipropellants. Hydroxylammonium nitrate (HAN)-based propellants are a viable and

    Hydroxylammonium nitrate

    Hydroxylammonium nitrate

    Hydroxylammonium_nitrate

  • Dummy round
  • Ammunition type used for training

    round is a round that is completely inert, i.e., contains no primer, propellant, or explosive charge (filling). It is used to check weapon function and

    Dummy round

    Dummy round

    Dummy_round

  • Arcjet rocket
  • Type of spacecraft electric propulsion system

    (arc) is created in a flow of propellant (typically hydrazine or ammonia). This imparts additional energy to the propellant, so that one can extract more

    Arcjet rocket

    Arcjet_rocket

  • Nitrous oxide fuel blend
  • Class of liquid rocket propellants

    Nitrous oxide fuel blend propellants are a class of liquid rocket propellants that were intended in the early 2010s to be able to replace hydrazine as

    Nitrous oxide fuel blend

    Nitrous_oxide_fuel_blend

  • Muzzle velocity
  • Velocity of projectile the moment it leaves the gun barrel

    tradeoff. A faster-burning propellant may accelerate a lighter projectile to higher speeds if the same amount of propellant is used. Within a gun, the

    Muzzle velocity

    Muzzle velocity

    Muzzle_velocity

  • Propellant 23 (The Avengers)
  • 2nd episode of the 2nd season of The Avengers

    "Propellant 23" is the second episode of the second series of the 1960s cult British spy-fi television series The Avengers, starring Patrick Macnee and

    Propellant 23 (The Avengers)

    Propellant_23_(The_Avengers)

  • Russo-Ukrainian war (2022–present)
  • Phase since 2022 of war ongoing since 2014

    provided Russia with geospatial intelligence, machine tools for tanks, and propellants for missiles. In September 2024, Reuters reported documents indicating

    Russo-Ukrainian war (2022–present)

    Russo-Ukrainian war (2022–present)

    Russo-Ukrainian_war_(2022–present)

  • High–low system
  • Design of cannon and anti-tank launcher

    anti-tank warfare launcher using a smaller high-pressure chamber to store propellant. It allows a much larger projectile to be launched without the heavy equipment

    High–low system

    High–low_system

  • Pulsed rocket motor
  • Solid-fuel rocket motor that can restart

    This design overcomes difficulties shutting down and reigniting solid propellant motors. The pulse rocket motor allows the motor to be burned in segments

    Pulsed rocket motor

    Pulsed_rocket_motor

  • Tripropellant rocket
  • Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially

    uses three propellants, as opposed to the more common bipropellant rocket or monopropellant rocket designs, which use two or one propellants, respectively

    Tripropellant rocket

    Tripropellant_rocket

  • Gas core reactor rocket
  • Rocket-propelled by exhausted coolant of a gas-cooled nuclear reactor

    relatively fast interplanetary travel. Heat transfer to the working fluid (propellant) is by thermal radiation, mostly in the ultraviolet, given off by the

    Gas core reactor rocket

    Gas_core_reactor_rocket

  • P160C
  • Solid-fuel first-stage rocket motor

    for 'powder'), referring to its solid propellant; "160" denotes the original target of 160 tonnes of propellant; and "C" signifies its common use across

    P160C

    P160C

    P160C

  • Spacecraft electric propulsion
  • Type of spacecraft propulsion using electrical energy to accelerate propellant

    spacecraft propulsion systems that use electric energy to accelerate and expel propellant, generating thrust through electric or magnetic fields. Their principal

    Spacecraft electric propulsion

    Spacecraft electric propulsion

    Spacecraft_electric_propulsion

  • Subcooling
  • Liquids below boiling point

    refrigeration cycles and steam turbine cycles. Some rocket engines use subcooled propellants. In refrigeration systems, subcooling the refrigerant is necessary to

    Subcooling

    Subcooling

  • Vikram-1
  • Indian small-lift launch vehicle developed by Skyroot Aerospace

    stages, while the fourth stage is a liquid stage, powered by hypergolic propellant. The first flight, known as Aagaman, flew on 18 July 2026. The launch

    Vikram-1

    Vikram-1

    Vikram-1

  • List of 40 mm grenades
  • Grenade suitable for use with a grenade launcher

    Milkor MGL, Heckler & Koch AG36 and M320 Grenade Launcher Module. The propellant has low pressure and gives the projectile an average velocity of 78–84 m/s

    List of 40 mm grenades

    List of 40 mm grenades

    List_of_40_mm_grenades

  • 1,1-Difluoroethane
  • Chemical compound

    formula C2H4F2 or CH3CHF2. This colorless gas is primarily used as a propellant and foam blowing agent as well as a component in a refrigerant, where

    1,1-Difluoroethane

    1,1-Difluoroethane

    1,1-Difluoroethane

  • Hall-effect thruster
  • Type of electric propulsion system

    thruster or Hall-current thruster) is a type of ion thruster in which the propellant is accelerated by an electric field. Based on the discovery by Edwin Hall

    Hall-effect thruster

    Hall-effect thruster

    Hall-effect_thruster

  • Improved military rifle powder
  • Propellants

    Improved military rifle propellants are tubular nitrocellulose propellants evolved from World War I through World War II for loading military and commercial

    Improved military rifle powder

    Improved military rifle powder

    Improved_military_rifle_powder

  • Cryogenic fuel
  • Fuels which require storage at very low temperatures to remain liquid

    storage tanks must be able to withstand high pressure. High-pressure propellant tanks require thicker walls and stronger alloys which make the vehicle

    Cryogenic fuel

    Cryogenic_fuel

  • Crawford burner
  • Solid rocket fuel burn rate tester

    A Crawford burner is a device used to test burn rate of solid propellants under different high-pressure conditions. It is also known as a Crawford bomb

    Crawford burner

    Crawford_burner

  • Hair spray
  • Hair styling product

    as a propellant. Hair sprays consist of the following components: concentrate, plasticizers, luster agents, and fragrances, as well as propellants. Hair

    Hair spray

    Hair spray

    Hair_spray

  • Passivation (spacecraft)
  • Removal of internal energy in a spaceship at end of its mission

    internal pressure when impacted. Passivation of propellant systems involves discharging remaining liquid propellant or pressurant gas into space. One proposed

    Passivation (spacecraft)

    Passivation_(spacecraft)

  • Starship HLS
  • Lunar lander variant of SpaceX Starship

    ship and the Starship depot—propellant depot that will remain in Earth orbit and collect/store the requisite propellant to refill the HLS ship before

    Starship HLS

    Starship HLS

    Starship_HLS

  • Solar thermal rocket
  • Theoretical spacecraft propulsion system

    they use solar power to heat up the propellant:[citation needed] Indirect solar heating involves pumping the propellant through passages in a heat exchanger

    Solar thermal rocket

    Solar_thermal_rocket

  • SpaceX Mars colonization program
  • Proposed human Mars program by SpaceX

    reliance on In situ resource utilization (ISRU) to synthesize return propellant would require massive surface power generation (likely nuclear) and water-mining

    SpaceX Mars colonization program

    SpaceX_Mars_colonization_program

  • Burn rate (chemistry)
  • Measure of the linear combustion rate of a substance

    combustion rate of a compound or substance such as a candle or a solid propellant. It is measured in length over time, such as millimeters per second or

    Burn rate (chemistry)

    Burn_rate_(chemistry)

  • In situ resource utilization
  • Astronautical use of materials harvested in outer space

    be brought from Earth. ISRU could provide materials for life support, propellants, construction materials, and energy to a spacecraft payloads or space

    In situ resource utilization

    In situ resource utilization

    In_situ_resource_utilization

  • Gravity assist
  • Space navigation technique

    object to alter the path and speed of a spacecraft, typically to save propellant and reduce expense. Gravity assistance can be used to accelerate a spacecraft

    Gravity assist

    Gravity assist

    Gravity_assist

  • Jack Parsons
  • American rocket engineer (1914–1952)

    invented the first rocket engine to use a castable, composite rocket propellant, and pioneered the advancement of both liquid-fuel and solid-fuel rockets

    Jack Parsons

    Jack Parsons

    Jack_Parsons

  • Cold gas thruster
  • Type of rocket engine

    of the propellant.[citation needed] Cold gas systems can use either a solid, liquid or gaseous propellant storage system; but the propellant must exit

    Cold gas thruster

    Cold_gas_thruster

  • SpaceX Starship (spacecraft)
  • Reusable spacecraft under development by SpaceX

    between the gaps in between the tiles to prevent heat seeping in. The propellant tanks on Starship are separated by a common bulkhead, similar to the ones

    SpaceX Starship (spacecraft)

    SpaceX Starship (spacecraft)

    SpaceX_Starship_(spacecraft)

  • Nitroglycerin
  • Chemical compound

    with nitrocellulose to form double-based smokeless powder, used as a propellant in artillery and firearms since the 1880s. As is the case for many other

    Nitroglycerin

    Nitroglycerin

    Nitroglycerin

  • SpaceX Super Heavy
  • Reusable first-stage rocket developed by SpaceX

    is powered by 33 Raptor engines that use liquid oxygen and methane as propellants. It returns to its launch site after propelling the second stage toward

    SpaceX Super Heavy

    SpaceX Super Heavy

    SpaceX_Super_Heavy

  • Muzzle flash
  • Light created by gunfire

    the blast and flash are products of the exothermic combustion of the propellant (gunpowder), and any remaining unburned powders reacting with ambient

    Muzzle flash

    Muzzle flash

    Muzzle_flash

  • Pulsed inductive thruster
  • Type of spacecraft plasma propulsion system

    engine using perpendicular electric and magnetic fields to accelerate a propellant with no electrode. A nozzle releases a puff of gas which spreads across

    Pulsed inductive thruster

    Pulsed inductive thruster

    Pulsed_inductive_thruster

  • Muzzle brake
  • Anti-recoil gunbarrel attachment

    barrel of a firearm or cannon that is intended to redirect a portion of propellant gases to counter recoil and unwanted muzzle rise. Barrels with an integral

    Muzzle brake

    Muzzle brake

    Muzzle_brake

  • Space Shuttle
  • Partially reusable launch system and space plane

    boosters, Class II would use multiple expendable rocket engines and a single propellant tank (stage-and-a-half), and Class III would have both a reusable orbiter

    Space Shuttle

    Space Shuttle

    Space_Shuttle

  • Apollo 11
  • First crewed Moon landing (1969)

    landing site had to be close to the lunar equator to minimize the amount of propellant required, clear of obstacles to minimize maneuvering, and flat to simplify

    Apollo 11

    Apollo 11

    Apollo_11

  • Williams spray equation
  • {\displaystyle x=0} respectively. Boltzmann equation Spray (liquid drop) Liquid-propellant rocket Smoluchowski coagulation equation Williams, F. A. (1958). "Spray

    Williams spray equation

    Williams_spray_equation

  • Fuel gas
  • Fuels which under ordinary conditions, are gaseous

    Fuel gas is one of a number of fuels that under ordinary conditions are gaseous. Most fuel gases are composed of hydrocarbons (such as methane and propane)

    Fuel gas

    Fuel gas

    Fuel_gas

  • Ho-301 cannon
  • Aircraft autocannon

    The propellant chamber is sealed by a thin aluminum sealing cup, which covers the exhaust holes. When the primer is struck, the bag of propellant ignites

    Ho-301 cannon

    Ho-301 cannon

    Ho-301_cannon

  • Solar sail
  • Space propulsion method using Sun radiation

    long operating lifetimes. Since they have few moving parts and use no propellant, they could potentially be used numerous times for the delivery of payloads

    Solar sail

    Solar sail

    Solar_sail

  • Regenerative cooling (rocketry)
  • Passing cold propellant through tubes around a rocket engine to cool it

    regenerative cooling is a configuration in which some or all of the propellant is passed through tubes, channels, or in a jacket around the combustion

    Regenerative cooling (rocketry)

    Regenerative_cooling_(rocketry)

  • Project Rover
  • U.S. project to build a nuclear thermal rocket

    by highly enriched uranium, with liquid hydrogen used as both a rocket propellant and reactor coolant. Nuclear graphite and beryllium were used as neutron

    Project Rover

    Project Rover

    Project_Rover

  • Starship flight test 13
  • Rocket flight test

    flight director conducts poll and verifies go for propellant load Go for propellant loading Go for propellant loading −00:37:30 Ship LOX (liquid oxygen) load

    Starship flight test 13

    Starship flight test 13

    Starship_flight_test_13

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