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See searches and references containing SPECIFIC THRUST!SPECIFIC THRUST
Specific thrust is the thrust per unit air mass flowrate of a jet engine (e.g. turbojet, turbofan, etc.) and can be calculated by the ratio of net thrust/total
Specific_thrust
Change in velocity per amount of fuel
propellant Specific energy Specific thrust—thrust per unit of air for a duct engine Standard gravity System-specific impulse Thrust specific fuel consumption—fuel
Specific_impulse
Fuel efficiency of an engine design with respect to thrust output
Thrust-specific fuel consumption (TSFC) is the fuel efficiency of an engine design with respect to thrust output. TSFC may also be thought of as fuel
Thrust-specific fuel consumption
Thrust-specific_fuel_consumption
Airbreathing jet engine designed to provide thrust by driving a fan
velocity, giving much more thrust per unit energy (lower specific thrust). Both airstreams contribute to the gross thrust of the engine. The additional
Turbofan
Aircraft propulsion system efficient at a range of speeds higher and lower than sound's
reduce aircraft drag at supercruise, SST engines require a high specific thrust (net thrust/airflow) to minimize the powerplant's cross-sectional area. This
Variable_cycle_engine
Reaction force
Thrust is a reaction force described quantitatively by Newton's third law. When a system expels or accelerates mass in one direction, the accelerated mass
Thrust
Turbojet engine component
mostly those on military supersonic aircraft. Its purpose is to increase thrust, usually for supersonic flight, takeoff, and combat. The afterburning process
Afterburner
Quotient of a quantity by mass
consumption per unit of braking power Thrust-specific fuel consumption, fuel consumption per unit of thrust Specific acid catalysis, in which the reaction
Specific_quantity
Electrothermal thruster in development
high thrust, low specific impulse chemical rockets and low thrust, high specific impulse electric propulsion, but has not yet demonstrated high thrust. The
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Type of jet engine
greater net thrust to be available at slow speeds. Thus civil turbofans today have a low exhaust speed (low specific thrust – net thrust divided by airflow)
Airbreathing_jet_engine
Non-airbreathing engine used to propel a missile or vehicle
engines typically have the highest thrust, but are the least propellant-efficient (they have the lowest specific impulse). For thermal rockets, pure
Rocket_engine
High-bypass turbofan aircraft engine
turbofan aircraft engines built by GE Aerospace for the Boeing 777, with thrust ratings from 81,000 to 115,000 pounds-force (360 to 510 kilonewtons). It
General_Electric_GE90
American low-bypass turbofan engine for the F-22 Raptor
and a fully variable convergent-divergent nozzle to achieve high specific thrust in intermediate, or non-afterburning power. The combustor, internally
Pratt_&_Whitney_F119
Aerodynamic phenomenon
the air to attain a higher temperature increasing the specific thrust. If the generated thrust is less than the aerodynamic drag of the ducting and radiator
Meredith_effect
Russian turbofan engine
well as 19% higher thrust-to-weight ratio, 6.4% better specific thrust, and 9% lower specific fuel consumption; estimated thrust is 107.9 kN (24,300 lbf)
Saturn_AL-51
SpaceX family of liquid-fuel rocket engines
000 lbf) thrust at sea level with a specific impulse of 330 s (3,200 m/s), with a nozzle exit diameter of 1.3 m (4.3 ft). Raptor Vacuum would have specific impulse
SpaceX_Raptor
Variable Pitch Propeller
of high bypass ratio turbofans. One of the methods used to reduce thrust-specific fuel consumption is to improve propulsive efficiency. This involves
Variable_pitch_fan
Turbofan aircraft engine
military transport turbofans. Ivchenko Lotarev chose a very low specific thrust (net thrust/airflow) cycle for the DV-2, so a single stage fan is sufficient
Lotarev_DV-2
In orbital mechanics, low-thrust relative transfer is an orbital maneuver in which a chaser spacecraft covers a specific relative distance relative to
Low thrust relative orbital transfer
Low_thrust_relative_orbital_transfer
Airliner faster than the speed of sound
regulators to disfavor the practice. SST engines need a fairly high specific thrust (net thrust/airflow) during supersonic cruise, to minimize engine cross-sectional
Supersonic_transport
Turbofan aircraft engine
unit) driven by a two-stage, air-cooled, HP turbine. This engine has a thrust-specific fuel consumption (TSFC) of 0.39 lb/(lbf⋅h) (11 g/(kN⋅s)) at static
Rolls-Royce_BR700
Canadian aerospace company
nozzle (PCT patent pending) contracts in the subsonic mode for optimal specific thrust. As the engine accelerates to supersonic velocities, the articulated
Space_Engine_Systems
Temporary diversion of an aircraft engine's thrust
Thrust reversal, also called reverse thrust, is an operating mode for jet engines equipped with a thrust reverser when thrust is directed forwards for
Thrust_reversal
Engine where combustion is pulsed instead of continuous
of construction, and high noise levels. While the thrust-to-weight ratio is excellent, thrust specific fuel consumption is very poor. The pulsejet uses
Pulsejet
Turbojet engine
high overall pressure ratio to help improve both thrust-specific fuel consumption and specific thrust, but it was known that throttling a single high-pressure-ratio
Pratt_&_Whitney_J57
Rocket engine in SpaceX Falcon launch vehicles
the Merlin 1C had a sea-level thrust of 350 kN (78,000 lbf), a vacuum thrust of 400 kN (90,000 lbf) and a vacuum specific impulse of 304 s (2.98 km/s)
SpaceX_Merlin
Liquid fuel rocket engine
electrically pump fed. He then stated that it had a thrust of 1 MN (220,000 lbf) and 320 seconds of specific impulse. The same day, the Neutron page on Rocket
Archimedes_(rocket_engine)
Rocket engine used on the Saturn V rocket
909 MN) Burn time: 159 seconds Specific impulse: 264.72 s (2.5960 km/s) Mixture ratio: 2.2674 S-IC total sea level liftoff thrust: 7,766,000 lbf (34.54 MN)
Rocketdyne_F-1
Aircraft engine that produces thrust by emitting a jet of gas
discharging a fast-moving jet of heated gas (usually air) that generates thrust by jet propulsion. While this broad definition may include rocket, water
Jet_engine
Conceptual space vehicle for interstellar travel
An interstellar ark is a conceptual starship designed for interstellar travel. Interstellar arks may be the most economically feasible method of traveling
Interstellar_ark
Jet engine where combustion takes place in supersonic airflow
{\displaystyle \eta _{0}} ), in terms of the specific impulse of the engine: η 0 = g 0 V 0 h PR I sp = Thrust power Chemical energy rate {\displaystyle \eta
Scramjet
Parameter in the gravitational two-body problem
the gravitational two-body problem, the specific orbital energy ε {\displaystyle \varepsilon } (or specific vis-viva energy) of two orbiting bodies is
Specific_orbital_energy
Hydrogen-oxygen rocket engine for the Delta IV
consequences of this simplicity were a significantly lower thrust-to-weight ratio and a 10% lower specific impulse compared to the SSME. The benefit of this simplicity
RS-68
Dimensionless ratio of thrust to weight of a propelled vehicle
Thrust-to-weight ratio is a dimensionless ratio of thrust to weight of a reaction engine or a vehicle with such an engine. Reaction engines include jet
Thrust-to-weight_ratio
Characteristic of rocket engine nozzles
and a specific impulse I s p {\displaystyle I_{sp}} can be found to characterize the overall efficiency of a rocket engine design. The thrust coefficient
Thrust_coefficient
Aircraft fuel efficiency
weight, and with improved engine brake-specific fuel consumption and propulsive efficiency or thrust-specific fuel consumption. Endurance and range can
Fuel_economy_in_aircraft
Rocket engine
(LOX) propellants, with each engine producing 1,033.1 kN (232,250 lbf) of thrust in vacuum. The engine's preliminary design dates back to recommendations
Rocketdyne_J-2
Type of propelling nozzle
generates forward thrust. Specific impulse is often expressed as a product of characteristic velocity c ∗ {\displaystyle c^{*}} and thrust coefficient C F
Rocket_engine_nozzle
Turbine engine driving an aircraft propeller
major portion of the total thrust, since almost all of the engine's power is used to drive the propeller. Exhaust thrust in a turboprop is sacrificed
Turboprop
Airbreathing jet engine which is typically used in aircraft
the propelling nozzle where it is accelerated to high speed to provide thrust. Two engineers, Frank Whittle in the United Kingdom and Hans von Ohain in
Turbojet
Proportion of ducted compared to combusted air in a turbofan engine
fuel consumption for the same thrust, measured as thrust specific fuel consumption (grams/second fuel per unit of thrust in kN using SI units). Lower fuel
Bypass_ratio
Measure of efficiency in aerospace engineering
capabilities of various vehicles Specific fuel consumption (thrust) – Fuel efficiency of an engine design with respect to thrust outputPages displaying short
Propulsive_efficiency
Chiropractic technique
and singular to the chiropractic profession ... characterized by a specific thrust applied to the vertebra utilizing parts of the vertebra and contiguous
Spinal_adjustment
Airliner concept
exhaust velocity increases the propulsive efficiency with a similar specific thrust. By ingesting and reenergizing the boundary layer flow, BLI reduces
Aurora_D8
American variable-cycle turbofan engine
Advanced Tactical Fighter (ATF) program. It was designed to produce maximum thrust in the 35,000 lbf (156 kN) class. Prototype engines were installed in the
General_Electric_YF120
Type of electric propulsion system
accelerate the ions to produce thrust, and neutralize the ions in the plume. The Hall-effect thruster is classed as a moderate specific impulse (1,600 s) space
Hall-effect_thruster
Type of rocket engine
oxygen as propellants, generating an average thrust of 518 N (116 lbf) and delivering 290 seconds of specific impulse. Rotating combustion also created a
Rotating_detonation_engine
High-thrust turbofan jet engine
a 5% lower thrust specific fuel consumption (TSFC) than the XWB-97 with maintenance costs comparable to the GE90-115B. The initial thrust of 105,000 lbf
General_Electric_GE9X
Soviet super heavy-lift launch vehicle (1965–1972)
most powerful rocket stage flown for over 50 years, at 45 meganewtons of thrust, until the SpaceX Super Heavy. Block A's large cluster of thirty NK-15 engines
N1_(rocket)
Form of electric spacecraft propulsion
Where: F is the thrust force in N, η is the efficiency P is the electrical power used by the thruster in W, and Isp is the specific impulse in seconds
Ion_thruster
Supersonic atmospheric jet engine
Ramjets generally give little or no thrust below about half the speed of sound, and they are inefficient (specific impulse of less than 600 seconds) until
Ramjet
Space Shuttle and SLS main engine
operational history to improve the engine's thrust, reliability, safety, and maintenance load. The engine produces a specific impulse (Isp) of 452 seconds (4.43 kN⋅s/kg)
RS-25
Solid propellant rocket used by the Space Shuttle
for human spaceflight. The two SRBs provided 85% of the Space Shuttle's thrust at liftoff and for the first two minutes of ascent. After burnout, they
Space Shuttle Solid Rocket Booster
Space_Shuttle_Solid_Rocket_Booster
Gas turbine used to spin a shaft
gas turbine that is optimized to produce shaft horsepower rather than jet thrust. In concept, turboshaft engines are very similar to turbojets, with additional
Turboshaft
Thrust produced by ejecting a jet of fluid
Isp = 3600/SFC for SFC in lb/(lbf·hr). From the definition of specific impulse thrust in SI units is: F = m ˙ V e {\displaystyle F={\dot {m}}V_{e}} where
Jet_propulsion
Study to reduce aircraft noise dramatically
proposed. The favoured engine configuration was a turbofan with very low specific thrust, i.e. very high ratio of bypass air. This gives a less effective exhaust
Silent_Aircraft_Initiative
Soviet (now Russian) rocket engine, the most powerful in the world
instability while designing bigger thrust chambers. At that time, they solved the problem by using a cluster of smaller thrust chambers. The RD-170 engine featured
RD-170
Rocket engine that uses liquid fuels and oxidizers
temperatures. Most designs of liquid rocket engines are throttleable for variable thrust operation. Some allow control of the propellant mixture ratio (ratio at
Liquid-propellant_rocket
Topics referred to by the same term
efficiency within a shaft engine Thrust-specific fuel consumption, fuel efficiency of an engine design with respect to thrust output This disambiguation page
Specific_fuel_consumption
Measure of amount of effort to change trajectory
required, though the specific kinetic and potential energies in the final orbit and the initial orbit are equal. When rocket thrust is applied in short
Delta-v
Chemical or mixture used in a rocket engine
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, as
Rocket_propellant
Type of engine
A reaction engine is an engine or motor that produces thrust by expelling reaction mass (reaction propulsion), in accordance with Newton's third law of
Reaction_engine
Proposed Soviet rocket engine
burns 27.4 kg/s of hydrogen, and 148 kg/s of oxygen. Thrust reduces to 1.6 MN, but the specific impulse increases to 460s. RD-170 - RP-1/LOX Russian engine
RD-701
Aircraft propulsion component
expressed slightly differently in terms of thrust and torque since the required output of the propeller is thrust. Thrust and torque are the basis of the definition
Propeller_(aeronautics)
Type of electric propulsion
propulsion that generates thrust from a quasi-neutral plasma. This is in contrast with ion thruster engines, which generate thrust through extracting an ion
Plasma_propulsion_engine
Type of rocket engine
is to direct the exhaust of a rocket engine in one direction, generating thrust in the opposite direction. The exhaust, a high-temperature mix of gases
Aerospike_engine
Chinese super-heavy rocket in development
tons. 16 YF-135 liquid oxygen kerosene engines, each with over 300 tons of thrust, will be used in the first stage; 120-ton hydrogen-oxygen engines will be
Long_March_9
Manual control of the thrust of an aircraft's engines from the cockpit
Thrust levers or throttle levers are found in the cockpit of aircraft, and are used by the pilot, copilot, flight engineer, or autopilot to control the
Thrust_lever
Empowerment of individuals regarding issues involving the law
legal aid centres may provide for limited legal literacy related to specific thrust areas. China conducts Nationwide Legal Awareness Raising Campaigns
Legal_awareness
Russian rocket engine
The RD-107 has an additional two vernier combustion chambers that can thrust vector in a single plane to supply attitude control. The RD-108 has four
RD-107
Type of aircraft engine
propfans with a specific fuel burn of 0.46 kg/kg-thrust/hour, a cruise thrust of 1.6 tonnes-force (3,500 lbf; 16 kN), and a static thrust of 8 to 9 tf (18
Propfan
organizations use the nomenclature of average thrust and burning time. The designation for a specific motor looks like C6-3. In this example, the letter
Model rocket motor classification
Model_rocket_motor_classification
Liquid-fueled rocket engine
thrust and 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
Rutherford_(rocket_engine)
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
Method used to accelerate spacecraft
result in technical solutions that improve thrust levels, specific impulse, power, specific mass, (or specific power), volume, system mass, system complexity
Spacecraft_propulsion
Large Soviet rocket engine that used hypergolic propellants
problems but increased the specific impulse of the engine by 42 seconds (0.41 km/s). The engine throttle range was 95–105%, the thrust vector control range
RD-270
Indian government laboratory
basic research, technology development and commercialization; have specific thrusts on frontier areas of research, National Mission Projects, regional
National Institute for Interdisciplinary Science and Technology
National_Institute_for_Interdisciplinary_Science_and_Technology
Type of rocket engine
generate thrust. As opposed to traditional rocket engines, a cold gas thruster does not house any combustion and therefore has lower thrust and efficiency
Cold_gas_thruster
Ion thruster subtype
its benefits include high efficiency, thrust density, and specific impulse; however it has very low total thrust, on the order of micronewtons. It provides
Colloid_thruster
Part of the Redstone rocket family
(64 kg) Propulsion Stage 1: 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
Jupiter-C
Soviet designed rocket family
included lower stage modifications to reduce structural mass, increase thrust, and fully use propellants. Generally a Briz-M (Russian: Бриз meaning Breeze)
Proton_(rocket_family)
Synergetic Air Breathing Rocket Engine - a proposed hybrid ramjet and rocket engine
hydrogen. The high pressure ratio would allow the engine to provide high thrust at very high speeds and altitudes. The low temperature of the air would
SABRE_(rocket_engine)
(660 lbf) of thrust with a chamber pressure of 880 kPa (128 psi) and a nozzle expansion of 153.8 that enables it to achieve a specific impulse of 302 s
KTDU-80
Model of aircraft performance
the total of kinetic and potential energies or aircraft specific energy. It relates the thrust, weight, aerodynamic drag, wing area, and other flight characteristics
Energy–maneuverability_theory
Unit of force
kilogram and meter as base units. The term pound of thrust is an alternative name for pound-force in specific contexts. It is frequently seen in US sources
Pound_(force)
Chinese super-heavy carrier rocket
Space Agency (CMSA). In 2020, a full-scale structural prototype of the thrust-transfer structure for the seven-engine first stage completed static load
Long_March_10
Indian expendable launch vehicle
providing 4846 kN of thrust. Within T+1, 4 out of the 6 boosters ignite on ground, each producing 703 kN of thrust. 7658 kN of total thrust is produced by the
Polar Satellite Launch Vehicle
Polar_Satellite_Launch_Vehicle
Japanese hydrolox staged combustion rocket engine
nozzle: Rated thrust (sea level): 843 kN (190,000 lbf) Rated thrust (vacuum): 1,074 kN (241,000 lbf) Specific impulse (sea level): Specific impulse (vacuum):
LE-7
Family of jet engines
000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust. Specific fuel consumption at 1,200 lbf (5,300 N) thrust (SLS, ISA) is understood to be 0.486 lb/(lbf⋅h)
Williams_FJ33
Russian heavy-lift launch vehicle
operate at full thrust for approximately 214 seconds, then separate. The URM-1 forming the vehicle's core is operated at full thrust for lift off, then
Angara_A5
Aircraft cockpit with electronic displays
pressure ratio Propulsive efficiency Specific impulse Thrust Thrust lapse Thrust specific fuel consumption Thrust to weight ratio Variable cycle engine
Glass_cockpit
Science fiction tabletop game
Full Thrust is a science fiction strategy wargame written by Jon Tuffley and published by Ground Zero Games of England. It is usually played with miniature
Full_Thrust
Type of nuclear thermal rocket
and presented at the 2016 AIAA/SAE/ASEE Propulsion Conference for thrust and specific impulse (Isp) amplification in a conventional nuclear thermal rocket
Pulsed_nuclear_thermal_rocket
Rocket engine that uses photons to propel a spacecraft
power sources would be required to provide reasonable thrust without unreasonable weight. The specific impulse of a photonic rocket is harder to define, since
Nuclear_photonic_rocket
Spacecraft launch or descent maneuver
optimization that uses gravity solely through the vehicle's own thrust. First, the thrust is not used to change the spacecraft's direction, so more of it
Gravity_turn
Conceptual rocket engine
resulting in a propulsion system characterized by high specific power, variable thrust, specific impulse, and minimal radiation emissions of spacecraft
Direct_Fusion_Drive
US project, 1987–1991, to develop nuclear thermal rocket engines
offered just over 1⁄3 the thrust from an engine of only 1650 kg (less than 1⁄4 the mass), while further improving the specific impulse from 930 to 1000
Project_Timberwind
One of the largest rocket engines to be designed
developed during the 1950s by the US Air Force. The M-1 offered a baseline thrust of 1,500,000 pounds-force (6.67 meganewtons) and an immediate growth target
Aerojet_M-1
American aerospace engineer (born 1938)
combustion. Researchers wrote that the design has higher efficiency and specific thrust than conventional designs, in which it is placed upstream of the turbine
William_Sirignano
Hypothetical propulsion systems for interstellar travel
electro-osmosis (also electroosmotic flow). It allows for a high specific impulse and high thrust-to-power ratio as well as a high final velocity which makes
Theoretical spacecraft propulsion
Theoretical_spacecraft_propulsion
SPECIFIC THRUST
SPECIFIC THRUST
Surname or Lastname
English
English : habitational name from any of the numerous places named in Old English as ‘long ford’, from lang, long ‘long’ + ford ‘ford’, except for Langford in Nottinghamshire, which is named with an Old English personal name Landa or possibly land, here used in a specific sense such as ‘boundary’ or ‘district’, with the same second element.
Surname or Lastname
English (chiefly Kent and Sussex)
English (chiefly Kent and Sussex) : occupational name for a designer or engineer, from a Middle English reduced form of Old French engineor ‘contriver’ (a derivative of engaigne ‘cunning’, ‘ingenuity’, ‘stratagem’, ‘device’). Engineers in the Middle Ages were primarily designers and builders of military machines, although in peacetime they might turn their hands to architecture and other more pacific functions.German : from the Latin personal name Januarius (see January 1). Jänner is a South German word for ‘January’, and so it is possible that this is one of the surnames acquired from words denoting months of the year, for example by converts who had been baptized in that month, people who were born or baptized in that month, or people whose taxes were due in January.
Girl/Female
Arabic
Precious; Lord of Specific Wood
Girl/Female
Biblical
A body thrust hard together.
Boy/Male
Indian, Sanskrit
Calmed; Pacific Sea
Boy/Male
Hindu
One of krishnas incarnations. specific to education
Surname or Lastname
English
English : metathesized variant of Thurston 1.
Surname or Lastname
English
English : habitational name from Brill in Buckinghamshire, named with the Celtic element bre- ‘hill’ + Old English hyll also ‘hill’.North German and Dutch : habitational name from any of various places in northwestern Germany and the Netherlands named Brill, from Middle Low German brūl, bröil ‘wet lowland’. Compare German Bruehl.German : from Middle Low German brill ‘eyeglasses’, hence a metonymic occupational name for a maker of spectacles or perhaps a nickname for someone who wore them.Jewish (Ashkenazic) : acronymic surname from Hebrew ben rabi ‘son of …’ and the first letter of each part of a Yiddish double male personal name, most likely Yude (Juda) Leyb. Many Ashkenazic family names beginning with Br- and Bar- are probably of acronymic origin, but without detailed evidence from family histories it is impossible to specify the personal name from which each is derived.
Boy/Male
Tamil
Prahalathan | பà¯à®°à®¹à®²à®¾à®¤à®¨
No specific meaning. but he was considered to be the best disciple in indian mythology
Prahalathan | பà¯à®°à®¹à®²à®¾à®¤à®¨
Boy/Male
Tamil
Hayagriv | ஹயாகà¯à®°à®¿à®µ
One of krishnas incarnations. specific to education
Hayagriv | ஹயாகà¯à®°à®¿à®µ
Girl/Female
American, Australian, Christian, Nigerian
Flaxen; Pacific Islander
Biblical
a body thrust hard together
Surname or Lastname
English
English : nickname from Middle English shouere ‘pusher’, an agent derivative of Old English scūfan ‘to thrust or push’.
Surname or Lastname
Variant of Dutch Schave.English
Variant of Dutch Schave.English : nickname from Middle English schove, probably from Old English scufa, a derivative of scūfan ‘to thrust or push’.
Girl/Female
Hindu, Indian, Malayalam, Marathi, Sanskrit, Sikh, Tamil
Aim; Destination; Who has a Specific Goal Everywhere; Target
Surname or Lastname
English
English : patronymic from Deemer.French : habitational name apparently associated with a specific domain; the source is unclear, because of the wide range of local variants.
Girl/Female
Indian, Telugu
Thrust
Boy/Male
Hindu
No specific meaning. but he was considered to be the best disciple in indian mythology
Surname or Lastname
German
German : eastern variant of Drescher.English : from an agent derivative of Middle English dressen ‘to arrange’ (in certain specific senses), possibly an occupational name for someone who dressed or finished cloth. Compare Fuller.
SPECIFIC THRUST
SPECIFIC THRUST
Surname or Lastname
North German
North German : probably from a nickname for someone who was spiteful or stubborn, from Middle Low German puch ‘defiance’.German : from a short form of a medieval personal name such as Burkhart.Respelling of Jewish (eastern Ashkenazic) Puk, a habitational name for someone from Puki, in Belarus.English : nickname from Middle English puck, pook ‘goblin’, ‘mischievous sprite’.
Boy/Male
Muslim
Patience
Male
English
Variant spelling of English Derek, DERRICK means "first of the people; king of nations."
Boy/Male
Latin
Manager.
Boy/Male
Tamil
Arunthiran | à®…à®°à¯à®¨à¯à®¤à¯€à®°à®£Â
Girl/Female
Arabic
Good Straight Path
Biblical
muddy; eggs; fine linen or silk
Boy/Male
Christian & English(British/American/Australian)
Fifth Child
Boy/Male
Egyptian
War.
Girl/Female
American, Australian, German, Hebrew
Close to God
SPECIFIC THRUST
SPECIFIC THRUST
SPECIFIC THRUST
SPECIFIC THRUST
SPECIFIC THRUST
v. t.
Proper station; specific place; assigned position; special location.
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.
a.
Causing dryness.
n.
The quality or state of being specific.
imp. & p. p.
of Specify
n.
The specific sum levied or assessed.
a.
Anything having peculiar adaption to the purpose to which it is applied.
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.
n.
A specific remedy. See Specific, a., 3.
p. pr. & vb. n.
of Specify
n.
The quality of being specific.
n.
An instrument for ascertaining the specific gravity of bodies.
a.
Specific.
n.
An instrument for ascertaining the specific gravity of liquids.
n.
A specific sum of money
a.
Specifying; definite, or making definite; limited; precise; discriminating; as, a specific statement.
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.
n.
Counseling to perform a specific illegal act.
adv.
In a specific manner.
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.