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SYSTEM SPECIFIC-IMPULSE

  • System-specific impulse
  • System-specific Impulse, Issp is a measure that describes performance of jet propulsion systems. A reference number is introduced, which defines the total

    System-specific impulse

    System-specific_impulse

  • Specific impulse
  • Change in velocity per amount of fuel

    Specific impulse (usually abbreviated as Isp) is a physical quantity defined as the ratio of change in momentum (impulse) to the mass used, usually fuel

    Specific impulse

    Specific_impulse

  • Impulse response
  • Output of a dynamic system when given a brief input

    impulse response, or impulse response function (IRF), of a dynamic system is its output when presented with a brief input signal, called an impulse (δ(t))

    Impulse response

    Impulse response

    Impulse_response

  • Variable Specific Impulse Magnetoplasma Rocket
  • Electrothermal thruster in development

    The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an electrothermal thruster under development for possible use in spacecraft propulsion.

    Variable Specific Impulse Magnetoplasma Rocket

    Variable Specific Impulse Magnetoplasma Rocket

    Variable_Specific_Impulse_Magnetoplasma_Rocket

  • Impulse
  • Topics referred to by the same term

    respect to time Impulse function, a mathematical function of an infinitely high amplitude and infinitesimal duration Impulse response, a system's output when

    Impulse

    Impulse

  • Project Orion (nuclear propulsion)
  • Discontinued US research program on the viability of nuclear pulse propulsion

    both at once (see spacecraft propulsion for more speculative systems). Specific impulse (Isp) measures how much thrust can be derived from a given mass

    Project Orion (nuclear propulsion)

    Project Orion (nuclear propulsion)

    Project_Orion_(nuclear_propulsion)

  • Impulse (physics)
  • Integral of a comparatively larger force over a short time interval

    In classical mechanics, impulse (symbolized by J or Imp) is the change in momentum of an object. It is most often used to describe forces which act over

    Impulse (physics)

    Impulse (physics)

    Impulse_(physics)

  • General Atomics
  • American defense and energy company

    2005. Retrieved September 21, 2016. Ross, F.W. (1960). Propulsive System Specific Impulse. General Atomics GAMD-1293 8 Feb. 1960. San Diego, California,

    General Atomics

    General_Atomics

  • Impulse Space
  • American space company

    with propellant. It uses Saiph bipropellant thrusters which have a specific impulse (Isp) of 290 s. It can impart a delta-v of from 500 m/s with 300 kg

    Impulse Space

    Impulse_Space

  • Infinite impulse response
  • Property of many linear time-invariant (LTI) systems

    Infinite impulse response (IIR) is a fundamental property applying to many linear time-invariant systems that are distinguished by having an impulse response

    Infinite impulse response

    Infinite_impulse_response

  • Beam-powered propulsion
  • Mechanism where confined high-speed particles confer energy to a vehicle

    propulsion system's specific impulse and thrust/weight ratio relative to conventional rocket propulsion. For example, hydrogen can provide a specific impulse of

    Beam-powered propulsion

    Beam-powered_propulsion

  • Scramjet
  • Jet engine where combustion takes place in supersonic airflow

    {\displaystyle I_{\text{sp}}} is the specific impulse h PR {\displaystyle h_{\text{PR}}} is fuel heat of reaction Specific impulse is often used as the unit of

    Scramjet

    Scramjet

    Scramjet

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

    have reasonably high density and their combustion products have high specific impulse (Isp). This allows the volume of the propellant tanks to be relatively

    Liquid-propellant rocket

    Liquid-propellant rocket

    Liquid-propellant_rocket

  • Cold gas thruster
  • Type of rocket engine

    a high specific impulse, and a high specific impulse per unit volume of propellant should be considered. Overview of the specific impulses of propellants

    Cold gas thruster

    Cold_gas_thruster

  • Transient response
  • Response of a system to a change from an equilibrium state

    the equilibrium of the system. The impulse response and step response are transient responses to a specific input (an impulse and a step, respectively)

    Transient response

    Transient response

    Transient_response

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

    or one propellants, respectively. Tripropellant systems can be designed to have high specific impulse and have been investigated for single-stage-to-orbit

    Tripropellant rocket

    Tripropellant_rocket

  • Finite impulse response
  • Type of filter in signal processing

    In signal processing, a finite impulse response (FIR) filter is a filter whose impulse response (or response to any finite length input) is of finite

    Finite impulse response

    Finite_impulse_response

  • Ion thruster
  • Form of electric spacecraft propulsion

    the amount of specific power required compared to chemical rockets. Ion thrusters are therefore able to achieve high specific impulses. The drawback of

    Ion thruster

    Ion thruster

    Ion_thruster

  • Variable cycle engine
  • Aircraft propulsion system efficient at a range of speeds higher and lower than sound's

    airspeed. In effect the engine can operate at any point along the specific impulse (Isp) curve - high Isp at low speed or low Isp at high speed. It is

    Variable cycle engine

    Variable cycle engine

    Variable_cycle_engine

  • Jet propulsion
  • Thrust produced by ejecting a jet of fluid

    gravity (g0) converts specific impulse from the mass basis to the weight basis. A propulsion system with a higher specific impulse uses the mass of the

    Jet propulsion

    Jet propulsion

    Jet_propulsion

  • SpaceX Raptor
  • SpaceX family of liquid-fuel rocket engines

    Starship system. SpaceX [@SpaceX] (3 August 2024). "Performance stats of previous versions: Raptor 1 (sea level variant) Thrust: 185tf Specific impulse: 350s

    SpaceX Raptor

    SpaceX Raptor

    SpaceX_Raptor

  • Frequency response
  • Output as a function of input frequency

    domain, just as the impulse response characterizes systems in the time domain. In linear systems (or as an approximation to a real system, neglecting second-order

    Frequency response

    Frequency_response

  • Gridded ion thruster
  • Space propulsion system

    electrostatic ion thruster called HiPEP which will have higher efficiency, specific impulse, and a longer lifetime than NSTAR.[citation needed] In 2006, Aerojet

    Gridded ion thruster

    Gridded ion thruster

    Gridded_ion_thruster

  • Pulsejet
  • Engine where combustion is pulsed instead of continuous

    propulsion, but usually have a poor compression ratio, and hence give a low specific impulse. The two main types of pulsejet engines use resonant combustion and

    Pulsejet

    Pulsejet

    Pulsejet

  • Nuclear pulse propulsion
  • Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust

    Space Shuttle main engine. With refinements a theoretical maximum specific impulse of 100,000 s (980 km/s) (1 MN·s/kg) might be possible. Thrusts were

    Nuclear pulse propulsion

    Nuclear pulse propulsion

    Nuclear_pulse_propulsion

  • RD-701
  • Proposed Soviet rocket engine

    388.4 kg/s (81.4% of propellant mass) of oxygen, achieving a with a specific impulse of 415s In high-altitude mode two, the preburner used to pump kerosene

    RD-701

    RD-701

  • Plasma propulsion engine
  • Type of electric propulsion

    interplanetary missions due to their high specific impulse. Many space agencies developed plasma propulsion systems, including the European Space Agency,

    Plasma propulsion engine

    Plasma propulsion engine

    Plasma_propulsion_engine

  • Dual-Stage 4-Grid
  • Type of electrostatic ion thruster

    energy input rate, the thruster could produce a thrust of 2.5 N. The specific impulse (a measure of fuel efficiency), could reach 19,300 s at an exhaust

    Dual-Stage 4-Grid

    Dual-Stage_4-Grid

  • Microwave electrothermal thruster
  • Type of space propulsion using microwaves

    in meters^2(m^2). Specific impulse is how efficiently the fuel of the MET is used to create thrust. The formula for specific impulse is given as: I s p

    Microwave electrothermal thruster

    Microwave_electrothermal_thruster

  • Rutherford (rocket engine)
  • Liquid-fueled rocket engine

    has a specific impulse of 311 s (3.05 km/s), while the vacuum optimized-version produces 25.8 kN (5,800 lbf) of thrust and has a specific impulse of 343 s

    Rutherford (rocket engine)

    Rutherford_(rocket_engine)

  • Afterburner
  • Turbojet engine component

    diluted with air from the compressor to bring the gas temperature down to a specific value, known as the Turbine Entry Temperature (TET) (1,570 °F (850 °C))

    Afterburner

    Afterburner

    Afterburner

  • Air-start system
  • Power source for starting large engines

    An air-start system is a power source used to provide the initial rotation to start large diesel engines and gas turbines. Compared to a gasoline (petrol)

    Air-start system

    Air-start_system

  • Resistojet rocket
  • Method of spacecraft propulsion

    300 °C in such a way results in a 41% increase in specific impulse. If heated by 900 °C, specific impulse could be doubled in comparison to a cold gas thruster

    Resistojet rocket

    Resistojet_rocket

  • RS-25
  • Space Shuttle and SLS main engine

    reliability, safety, and maintenance load. The engine produces a specific impulse (Isp) of 452 seconds (4.43 kN⋅s/kg) in vacuum, or 366 seconds (3.59 kN⋅s/kg)

    RS-25

    RS-25

    RS-25

  • Jet fuel
  • Type of aviation fuel

    on petroleum source, it is impossible to define jet fuel as a ratio of specific hydrocarbons. Jet fuel is therefore defined as a performance specification

    Jet fuel

    Jet fuel

    Jet_fuel

  • Solar electric propulsion
  • High efficiency engine for space travel

    Research Organisation (ISRO) and NASA. SEP has a significantly higher specific impulse than chemical rocket propulsion, thus requiring less propellant mass

    Solar electric propulsion

    Solar electric propulsion

    Solar_electric_propulsion

  • Model rocket motor classification
  • rockets) are classified by total impulse into a set of letter-designated ranges, from 1⁄8A up to O. The total impulse is the integral of the thrust over

    Model rocket motor classification

    Model_rocket_motor_classification

  • SpaceX Merlin
  • Rocket engine in SpaceX Falcon launch vehicles

    sea level and 420 kN (95,000 lbf) in vacuum, and performing with a specific impulse of 261 s (2.56 km/s) at sea level and 303 s (2.97 km/s) in vacuum.

    SpaceX Merlin

    SpaceX Merlin

    SpaceX_Merlin

  • Flameout
  • Type of engine issue in aviation

    atmospheric or operational conditions are conducive to it, engine control systems usually provide a continuous ignition function. Igniters are normally used

    Flameout

    Flameout

  • Electronic centralised aircraft monitor
  • Avionics system developed by Airbus

    aircraft monitoring (ECAM) or electronic centralized aircraft monitoring is a system on Airbus aircraft that monitors aircraft functions and relays them to the

    Electronic centralised aircraft monitor

    Electronic centralised aircraft monitor

    Electronic_centralised_aircraft_monitor

  • Solar thermal rocket
  • Theoretical spacecraft propulsion system

    propellant temperatures and therefore higher specific impulses, approaching 1200 seconds. Even the lower specific impulse represents a significant increase over

    Solar thermal rocket

    Solar_thermal_rocket

  • Characteristic velocity
  • Measure of rocket performance

    exhaust velocity related to the specific impulse by: I s p = c g 0 {\displaystyle I_{sp}={\frac {c}{g_{0}}}} . Specific impulse and effective exhaust velocity

    Characteristic velocity

    Characteristic_velocity

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

    composite propellant (APCP). This mixture gave the solid rocket motors a specific impulse of 242 seconds (2.37 km/s) at sea level or 268 seconds (2.63 km/s)

    Space Shuttle Solid Rocket Booster

    Space Shuttle Solid Rocket Booster

    Space_Shuttle_Solid_Rocket_Booster

  • Ramjet
  • Supersonic atmospheric jet engine

    thrust below about half the speed of sound, and they are inefficient (specific impulse of less than 600 seconds) until the airspeed exceeds 1,000 kilometres

    Ramjet

    Ramjet

    Ramjet

  • Long March 9
  • Chinese super-heavy rocket in development

    while the 2011 design for LM9 was seen as matching the NASA's Space Launch System. On 23 April 2022, Long provided some updates on yet another new design

    Long March 9

    Long March 9

    Long_March_9

  • Pelton wheel
  • Type of turbine

    is an impulse-type water turbine invented by American inventor Lester Allan Pelton in the 1870s. The Pelton wheel extracts energy from the impulse of moving

    Pelton wheel

    Pelton wheel

    Pelton_wheel

  • 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

  • Rocketdyne J-2
  • Rocket engine

    after the conclusion of the Apollo program. The engine produced a specific impulse (Isp) of 421 seconds (4.13 km/s) in a vacuum (or 200 seconds (2.0 km/s)

    Rocketdyne J-2

    Rocketdyne J-2

    Rocketdyne_J-2

  • Engine-indicating and crew-alerting system
  • Type of alert system on aircraft

    An engine-indicating and crew-alerting system (EICAS) is an integrated system used in modern aircraft to provide aircraft flight crew with instrumentation

    Engine-indicating and crew-alerting system

    Engine-indicating and crew-alerting system

    Engine-indicating_and_crew-alerting_system

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

    the propellants by their exhaust velocity relative to the rocket (specific impulse). A rocket can be thought of as being accelerated by the pressure of

    Rocket propellant

    Rocket propellant

    Rocket_propellant

  • Rotating detonation engine
  • Type of rocket engine

    an average thrust of 518 N (116 lbf) and delivering 290 seconds of specific impulse. Rotating combustion also created a torque of 0.26 N·m, so a S-shaped

    Rotating detonation engine

    Rotating detonation engine

    Rotating_detonation_engine

  • NASA Solar Technology Application Readiness
  • Space propulsion system, electrostatic gridded ion thruster

    operation, with a thrust of 20-92 mN, a specific impulse of 19000-30500 N·s/kg (1950-3100 s) and a total impulse capability of 2.65 × 106 Ns on DS1. In

    NASA Solar Technology Application Readiness

    NASA Solar Technology Application Readiness

    NASA_Solar_Technology_Application_Readiness

  • HGM-25A Titan I
  • Early American intercontinental ballistic missile

    internal inertial guidance system. Later Atlas E/F models were equipped with what would have been the Titan I's guidance system The Titan I would be deployed

    HGM-25A Titan I

    HGM-25A Titan I

    HGM-25A_Titan_I

  • Turbojet
  • Airbreathing jet engine which is typically used in aircraft

    stages do not need cooling. In the first stage, the turbine is largely an impulse turbine (similar to a pelton wheel) and rotates because of the impact of

    Turbojet

    Turbojet

    Turbojet

  • Hall-effect thruster
  • Type of electric propulsion system

    ions in the plume. The Hall-effect thruster is classed as a moderate specific impulse (1,600 s) space propulsion technology and has benefited from considerable

    Hall-effect thruster

    Hall-effect thruster

    Hall-effect_thruster

  • LE-7
  • Japanese hydrolox staged combustion rocket engine

    000 lbf) Rated thrust (vacuum): 1,074 kN (241,000 lbf) Specific impulse (sea level): Specific impulse (vacuum): 429 seconds (4.21 km/s) Long nozzle: Rated

    LE-7

    LE-7

    LE-7

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

    core may be either a gas or plasma. They may be capable of creating specific impulses of 3,000–5,000 s (30 to 50 kN·s/kg, effective exhaust velocities 30

    Gas core reactor rocket

    Gas_core_reactor_rocket

  • Colloid thruster
  • Ion thruster subtype

    thrusters, its benefits include high efficiency, thrust density, and specific impulse; however it has very low total thrust, on the order of micronewtons

    Colloid thruster

    Colloid thruster

    Colloid_thruster

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

    by using nitrocellulose, improving the overall specific impulse. The aluminium improves specific impulse as well as combustion stability. High performing

    Solid-propellant rocket

    Solid-propellant rocket

    Solid-propellant_rocket

  • Turboshaft
  • Gas turbine used to spin a shaft

    power section consists of additional stages of turbines, a gear reduction system, and the shaft output. The gas generator creates the hot expanding gases

    Turboshaft

    Turboshaft

    Turboshaft

  • Bleed air
  • Aircraft gas turbine function

    used during descent and other low-power operations. Bleed air from that system can be utilized for internal cooling of the engine, cross-starting another

    Bleed air

    Bleed_air

  • Tip jet
  • Jet nozzle at the tip of some helicopter rotor blades

    provided by a separate engine, to create jet thrust. Other types use a system that functions similarly to the afterburner (reheat) on a conventional jet

    Tip jet

    Tip jet

    Tip_jet

  • Fission-fragment rocket
  • Type of nuclear propulsion method with an ultra high specific-inpulse

    fluid as working mass. The design can, in theory, produce very high specific impulse while still being well within the abilities of current technologies

    Fission-fragment rocket

    Fission-fragment_rocket

  • Aircraft engine starting
  • of the two magnetos used in a typical aero engine ignition system is fitted with an 'impulse coupling', a spring-loaded device which delays the spark until

    Aircraft engine starting

    Aircraft engine starting

    Aircraft_engine_starting

  • Antimatter propulsion spacecraft
  • Rockets using antimatter as their power source

    Machine Jerry M. Seitzman, 2003-2004 High Specific Impulse Superfluid and Nanotube Propulsion Device, System and Propulsion Method Michael Wallace, Joseph

    Antimatter propulsion spacecraft

    Antimatter propulsion spacecraft

    Antimatter_propulsion_spacecraft

  • Titan IIIE
  • Expendable launch system used by NASA

    also known as the Titan III-Centaur, was an American expendable launch system. Launched seven times between 1974 and 1977, it enabled several high-profile

    Titan IIIE

    Titan IIIE

    Titan_IIIE

  • Coffman engine starter
  • Piston engine starting system

    Coffman engine starter (also known as a "shotgun starter") was a starting system used on many piston engines in aircraft and armored vehicles of the 1930s

    Coffman engine starter

    Coffman engine starter

    Coffman_engine_starter

  • Newton-second
  • SI derived unit of impulse

    (also newton second; symbol: N⋅s or N s) is the unit of impulse in the International System of Units (SI). It is dimensionally equivalent to the momentum

    Newton-second

    Newton-second

    Newton-second

  • Eclipse (rocket)
  • Rocket under development by Firefly Aerospace and Northrop Grumman

    provide 7,161 kN (1,610,000 lbf) of thrust and has 305 seconds of specific impulse (Isp). This stage is designed to be reusable, though a de-rated and

    Eclipse (rocket)

    Eclipse_(rocket)

  • Flight recorder
  • Robust aircraft electronic recording device

    and avionic systems and then routes them to the FDR and, if installed, to the QAR. Information from the FDAU to the FDR is sent via specific data frames

    Flight recorder

    Flight recorder

    Flight_recorder

  • Compressor stall
  • Gas turbine phenomenon

    by better design and the use of hydromechanical and electronic control systems such as full authority digital engine control (FADEC). Modern compressors

    Compressor stall

    Compressor stall

    Compressor_stall

  • Magnetoplasmadynamic thruster
  • Form of electrically powered spacecraft propulsion

    [citation needed] As with other electric propulsion variations, both specific impulse and thrust increase with power input, while thrust per watt drops.

    Magnetoplasmadynamic thruster

    Magnetoplasmadynamic thruster

    Magnetoplasmadynamic_thruster

  • Long March 10
  • Chinese super-heavy carrier rocket

    landing legs; this tethered system involves the deployment of "hooks" by the stage which would be caught by a tensioned wire system on the ground. The first

    Long March 10

    Long March 10

    Long_March_10

  • NERVA
  • US Nuclear thermal rocket engine project (1956–1973)

    flight application and was able to operate at a specific impulse twice that of chemical rocket system[s]." The engine was deemed adequate for Mars missions

    NERVA

    NERVA

    NERVA

  • Propfan
  • Type of aircraft engine

    993 kgf; 42.90 and 9.74 kN) in static thrust and cruise with a thrust-specific fuel consumption (TSFC) of 0.240 and 0.519 lb/(lbf⋅h) (6.8 and 14.7 g/(kN⋅s))

    Propfan

    Propfan

    Propfan

  • Combustor
  • Part of a jet engine where fuel is burned

    combustor or combustion chamber is fed high-pressure air by the compression system. The combustor then heats this air at constant pressure as the fuel/air

    Combustor

    Combustor

  • NEXT (ion thruster)
  • Space propulsion system, a gridded electrostatic ion thruster

    5 kW power, when it has a specific impulse of 1320 seconds. The NEXT thruster has demonstrated, in ground tests, a total impulse of 17 MN·s, which as of

    NEXT (ion thruster)

    NEXT (ion thruster)

    NEXT_(ion_thruster)

  • Delta Cryogenic Second Stage
  • Japanese-American rocket stage

    Rocketdyne, which features an extendable carbon–carbon nozzle to improve specific impulse. The DCSS was designed by the National Space Development Agency of

    Delta Cryogenic Second Stage

    Delta Cryogenic Second Stage

    Delta_Cryogenic_Second_Stage

  • Cardiac conduction system
  • Aspect of heart function

    spontaneously generated by the SA node, the cardiac pacemaker. This electrical impulse is propagated throughout the right atrium, and through Bachmann's bundle

    Cardiac conduction system

    Cardiac conduction system

    Cardiac_conduction_system

  • Epsilon (rocket)
  • JAXA small-lift rocket family

    eight people at the launch site, compared with 150 people for earlier systems. The rocket has a mass of 91 t (90 long tons; 100 short tons) and is 24

    Epsilon (rocket)

    Epsilon (rocket)

    Epsilon_(rocket)

  • Next Generation Launch Vehicle
  • Class of Indian partially reusable launch vehicles under development by ISRO

    family of these vehicles are designed to replace currently operational systems like the PSLV and GSLV. Previously referred to as Unified Launch Vehicle

    Next Generation Launch Vehicle

    Next Generation Launch Vehicle

    Next_Generation_Launch_Vehicle

  • Impulse roller coaster
  • Form of roller coaster manufactured by Intamin

    An Impulse roller coaster is a form of a launched inverted roller coaster manufactured by Intamin. The first Impulse roller coaster appeared in Japan

    Impulse roller coaster

    Impulse roller coaster

    Impulse_roller_coaster

  • Microturbine
  • 25-500-kW internal combustion engine, typically Brayton cycle-type

    turboprop with a recuperator to improve efficiency from 10 to 30%, for a brake specific fuel consumption similar to a piston engine, but 30 kg (66 lb) lighter

    Microturbine

    Microturbine

  • Components of jet engines
  • Brief description of components needed for jet engines

    This article describes the components and systems found in jet engines. It uses two example engines; the type most familiar to the general public, the

    Components of jet engines

    Components of jet engines

    Components_of_jet_engines

  • Autothrottle
  • System that allows a pilot to control thrust without manually setting fuel flow

    attain a specific target indicated air speed, or the assigned power for different phases of flight. A/T and AFDS (Auto Flight Director Systems) can work

    Autothrottle

    Autothrottle

    Autothrottle

  • Project Timberwind
  • US project, 1987–1991, to develop nuclear thermal rocket engines

    only 1650 kg (less than 1⁄4 the mass), while further improving the specific impulse from 930 to 1000 seconds.[citation needed] In 1983, the Strategic Defense

    Project Timberwind

    Project_Timberwind

  • Nuclear photonic rocket
  • Rocket engine that uses photons to propel a spacecraft

    propulsion system could be created. An antimatter-matter powered photon rocket would (disregarding the shielding) obtain the maximum c specific impulse; for

    Nuclear photonic rocket

    Nuclear_photonic_rocket

  • Jupiter-C
  • Part of the Redstone rocket family

    Rocketdyne A-7 engine Thrust, 83,000 lbf (370 kN) burning time, 155 s specific impulse, 235 s (2.30 kN·s/kg) propellants, liquid oxygen, as oxidizer, and

    Jupiter-C

    Jupiter-C

    Jupiter-C

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

    {\displaystyle I_{\text{sp}}g_{0}} ) I sp {\displaystyle I_{\text{sp}}} is the specific impulse in dimension of time; g 0 {\displaystyle g_{0}} is standard gravity;

    Tsiolkovsky rocket equation

    Tsiolkovsky rocket equation

    Tsiolkovsky_rocket_equation

  • J-2X
  • Liquid-fueled rocket engine

    each engine producing 1,307 kN (294,000 lbf) of thrust in vacuum at a specific impulse (Isp) of 448 seconds (4.39 km/s). The engine's mass is approximately

    J-2X

    J-2X

    J-2X

  • Pulsed nuclear thermal rocket
  • Type of nuclear thermal rocket

    presented at the 2016 AIAA/SAE/ASEE Propulsion Conference for thrust and specific impulse (Isp) amplification in a conventional nuclear thermal rocket. The pulsed

    Pulsed nuclear thermal rocket

    Pulsed nuclear thermal rocket

    Pulsed_nuclear_thermal_rocket

  • Geosynchronous Satellite Launch Vehicle
  • Class of Indian medium-lift expendable launch vehicles, developed by ISRO

    Geosynchronous Satellite Launch Vehicle (GSLV) is a class of expendable launch systems operated by ISRO. GSLV has been used in eighteen launches since 2001. The

    Geosynchronous Satellite Launch Vehicle

    Geosynchronous Satellite Launch Vehicle

    Geosynchronous_Satellite_Launch_Vehicle

  • Axial compressor
  • Machine for continuous flow gas compression

    as in military jets. The airfoil profiles are optimized and matched for specific velocities and turning. Although compressors can be run at other conditions

    Axial compressor

    Axial compressor

    Axial_compressor

  • Aerospike engine
  • Type of rocket engine

    tested the LAS 25DA aerospike steam rocket engine for the Launch Assist System. Another spike engine concept model, by KSF Space and Interstellar Space

    Aerospike engine

    Aerospike engine

    Aerospike_engine

  • Arcjet rocket
  • Type of spacecraft electric propulsion system

    over 585 s average specific impulse at 2 kW. The ammonia-based ESEX arcjet on the ARGOS satellite operated with a specific impulse of 786.2 ± 43.0 s over

    Arcjet rocket

    Arcjet_rocket

  • Aircraft fuel system
  • Engine fuel systems in aircraft

    An aircraft fuel system allows the crew to pump, manage, and deliver aviation fuel to the propulsion system and auxiliary power unit (APU) of an aircraft

    Aircraft fuel system

    Aircraft_fuel_system

  • Saturn C-5N
  • Proposed NASA super heavy-lift launcher

    in-space 3rd stage, still hold a number of combined rocket thrust and specific impulse records. The concept of nuclear thermal rockets serving as the in-space

    Saturn C-5N

    Saturn_C-5N

  • Pacemaker
  • Medical device for artificially stimulating heart contractions

    based on the dynamic demand of the circulatory system. Others send out a fixed rate of impulses. A specific type of pacemaker, called an implantable

    Pacemaker

    Pacemaker

    Pacemaker

  • Specific speed
  • Measure of turbomachinery speed

    Well-designed efficient machines typically use the following values: Impulse turbines have the lowest ns values, typically ranging from 1 to 10, a Pelton

    Specific speed

    Specific_speed

  • RD-107
  • Russian rocket engine

    high-frequency vibrations inside the combustion chambers and increasing specific impulse by about 5 seconds (0.049 km/s), or five percent. Used on the Soyuz-FG

    RD-107

    RD-107

    RD-107

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Online names & meanings

  • KATIDA
  • Female

    Esperanto

    KATIDA

    Esperanto name KATIDA means "kitten-like."

  • Fenil
  • Boy/Male

    Christian, Gujarati, Hindu, Indian, Jain, Kannada, Sindhi, Tamil, Telugu

    Fenil

    Name of French Flower

  • Rogelim
  • Biblical

    Rogelim

    a foot or footman

  • Triveni
  • Girl/Female

    Gujarati, Hindu, Indian, Kannada, Malayalam, Marathi, Sanskrit, Telugu

    Triveni

    Confluence of Three Sacred Rivers

  • Constantinos
  • Boy/Male

    English

    Constantinos

    Steady

  • Nehchaltek
  • Boy/Male

    Indian, Punjabi, Sikh

    Nehchaltek

    One whose Faith in God is Steadfast

  • Richman
  • Boy/Male

    American, Australian, British, English

    Richman

    Powerful

  • Adheem
  • Boy/Male

    Muslim/Islamic

    Adheem

    The most great

  • Vishamaksh
  • Boy/Male

    Hindu, Indian, Marathi

    Vishamaksh

    Lord Shiva

  • Vijesh | வீஜேஷ
  • Boy/Male

    Tamil

    Vijesh | வீஜேஷ

    Victory

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SYSTEM SPECIFIC-IMPULSE

  • Specific
  • a.

    Anything having peculiar adaption to the purpose to which it is applied.

  • Restem
  • v. t.

    To force back against the current; as, to restem their backward course.

  • Specify
  • v. t.

    To mention or name, as a particular thing; to designate in words so as to distinguish from other things; as, to specify the uses of a plant; to specify articles purchased.

  • Specificalness
  • n.

    The quality of being specific.

  • Sister
  • n.

    One of the same kind, or of the same condition; -- generally used adjectively; as, sister fruits.

  • System
  • n.

    An assemblage of objects arranged in regular subordination, or after some distinct method, usually logical or scientific; a complete whole of objects related by some common law, principle, or end; a complete exhibition of essential principles or facts, arranged in a rational dependence or connection; a regular union of principles or parts forming one entire thing; as, a system of philosophy; a system of government; a system of divinity; a system of botany or chemistry; a military system; the solar system.

  • Specified
  • imp. & p. p.

    of Specify

  • Specific
  • a.

    Specifying; definite, or making definite; limited; precise; discriminating; as, a specific statement.

  • Systemic
  • a.

    Of or relating to a system; common to a system; as, the systemic circulation of the blood.

  • Restem
  • v. t.

    To stem, or move against; as, to restem a current.

  • Specific
  • a.

    Exerting a peculiar influence over any part of the body; preventing or curing disease by a peculiar adaption, and not on general principles; as, quinine is a specific medicine in cases of malaria.

  • Specific
  • n.

    A specific remedy. See Specific, a., 3.

  • Specifical
  • a.

    Specific.

  • System
  • n.

    An assemblage of parts or organs, either in animal or plant, essential to the performance of some particular function or functions which as a rule are of greater complexity than those manifested by a single organ; as, the capillary system, the muscular system, the digestive system, etc.; hence, the whole body as a functional unity.

  • Specifically
  • adv.

    In a specific manner.

  • Pacific
  • a.

    Of or pertaining to peace; suited to make or restore peace; of a peaceful character; not warlike; not quarrelsome; conciliatory; as, pacific words or acts; a pacific nature or condition.

  • Systemic
  • a.

    Of or pertaining to the general system, or the body as a whole; as, systemic death, in distinction from local death; systemic circulation, in distinction from pulmonic circulation; systemic diseases.

  • Sister
  • v. t.

    To be sister to; to resemble closely.

  • Specific
  • a.

    Of or pertaining to a species; characterizing or constituting a species; possessing the peculiar property or properties of a thing which constitute its species, and distinguish it from other things; as, the specific form of an animal or a plant; the specific qualities of a drug; the specific distinction between virtue and vice.

  • System
  • n.

    Regular method or order; formal arrangement; plan; as, to have a system in one's business.