SIMETRIUM .COM newton of thrust
1 N = 1 kg·m/s²
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N N F mg SYMBOL PLATE1 N = 1 kg·m/s²F = ṁ·vₑ + (pₑ − pₐ)·Aₑnozzle exit · Mach diamonds · thrust versus weight
Letter case
The newton is named after a person, so the symbol is a capital N and the name is written in lowercase: newton. Multiples: kN, MN.
Do not confuse
A «tonne of thrust» is not a mass but a tonne-force: 9 807 N. An engine with 200 tonnes of thrust gives 1.96 MN. In the SI, thrust is written only in newtons.
On the plate is a rocket lifting off at night. The letter N is cut into the skin, with a copper nozzle beneath it. A plume with Mach diamonds bursts from the exit — this is how the jet looks when the pressure at the nozzle exit is lower than the air pressure. Arrow F is the thrust, arrow mg is the weight; the rocket climbs as long as the first is longer than the second.
Quantity passport · rocket and space technology · thrust force

Newton of thrust

SI unit of force · N · 1 N = 1 kg·m/s² · rocket thrust in MN

A newton is the force that speeds up a kilogram by one metre per second every second. An apple of about 100 grams presses on your palm with a force of one newton. A rocket engine throws out hundreds of kilograms of gas per second at 3–4 km/s and gets millions of newtons of thrust — meganewtons.

Thrust has two terms: the momentum of the jet ṁ·vₑ and the pressure difference at the nozzle exit. That is why the same engine pulls less at ground level than in vacuum, and the shape of the nozzle decides where it works best. A rocket lifts off only if its thrust is greater than its weight; their ratio is the thrust-to-weight ratio.

NotationN · kN · MN
Definition1 N = 1 kg·m/s² — by Newton’s second law F = ma
ThrustF = ṁ·vₑ + (pₑ − pₐ)·Aₑ
Old units1 kgf = 9.80665 N · 1 tf = 9.807 kN · 1 lbf = 4.448 N
Liftoffthrust-to-weight ratio F / mg greater than 1 · rockets at launch 1.2–1.6
Typical valuesapple — 1 N · jet engine — hundreds of kN · liquid rocket engine — about 2 MN · heavy rocket — 30–70 MN
To the conversion To the launch pad
01 · Definition

Force, jet momentum and exit pressure

Newton’s second law: force equals mass times acceleration. A newton is the force that gives a kilogram an acceleration of 1 m/s². An engine pushes off its own jet: every second it throws out a mass ṁ at a velocity vₑ and gets a force ṁ·vₑ — by the third law.

The second term is pressure. If the gas at the nozzle exit presses harder than the air, it still pushes; if weaker, the air squeezes the jet and takes away thrust. A long nozzle accelerates the gas more and works well in vacuum, but loses at ground level. A short one is the opposite. Specific impulse Isp is thrust per weight of propellant used per second, in seconds: the higher it is, the more economical the engine.

F — thrust · ṁ — mass flow, kg/s · vₑ — exhaust velocity · pₑ, pₐ — exit and ambient pressure · Aₑ — exit area · g₀ = 9.80665 m/s² · m₀, m₁ — mass before and after the burn
Interactive · thrust versus weight

How many newtons it takes to lift off

Choose what to lift and set the thrust — the scale is logarithmic, from 0.1 N to 100 MN. Weight is the force of gravity mg. Liftoff happens when thrust is greater than weight.

Thrust
Thrust
Weight mg
Thrust-to-weight ratio
Upward acceleration

Interactive · garage

Garage: build a rocket from parts

The rocket stands in the assembly hall. Every part changes the mass, the air drag and the thrust: the fairing sets the shape of the nose, the fuselage the diameter of the tanks and how many engines fit, the fins the stability at max-Q, the engine and the nozzle the thrust and specific impulse. The part changed last is highlighted. On the right are the mass by parts, the thrust-to-weight ratio and the Δv budget. When the rocket is ready — «Roll out to the pad».

Rocket parts
Fairing
Fuselage · diameter
Fins
Second stage
Trajectory
Engine · propellant
Nozzle
Engines
Fuel
Payload

Interactive · rocket builder and launch

Build a rocket — and see whether it lifts off

The rocket is built in the garage above: fairing, fuselage, fins, engines, nozzle, propellant and payload. Whatever is built rolls out to the pad. The main action is «Launch»: countdown, ignition, liftoff, the sound barrier, maximum dynamic pressure, engine cutoff and coasting up to the highest point. In the garage you can add a second stage and turn on «Turn to orbit»: after liftoff the rocket pitches over towards the horizon, the first stage separates, the second gains about 7.8 km/s sideways — and if the perigee is above 160 km, the rocket is in orbit. Without the turn the flight is vertical, like a sounding rocket. The first seconds run slowly, after that the flight is sped up; the slider under the scene rewinds it. On the right is a cutaway nozzle: exit pressure against ambient pressure, which set the shape of the jet and the thrust.

left: console — time, altitude, speed, thrust, g-load, mass, dynamic pressureright: nozzle and pressures, Δv budget
Main action
RewindT−3
Builder’s forecast
F / mg
Δv
mass
Altitude
—
—
Thrust
—
—
G-load
—
—
Flight summary
—
—

—

Thrust and weight
MN over flight time
Red is thrust: it grows with altitude because the air pressure falls. Blue is weight: it falls because the propellant burns. The difference between them is what accelerates the rocket.
Altitude and speed
km and km/s
The dashed line is the Kármán line, 100 km, the conventional edge of space. After engine cutoff the speed falls while the altitude keeps growing up to the highest point.
G-load and dynamic pressure
g and kPa
Dynamic pressure ½ρv² is how hard the oncoming air presses; its peak, max-Q, is the most dangerous moment for the airframe. The g-load grows towards the end of the burn: the propellant runs out, but the thrust stays the same.
02 · Conversion
In newtons

Quick estimate: a tonne-force is almost 10 kN, a hundred tonnes of thrust is about 1 MN. More precisely, multiply by 9.807.

American engines are often described in pounds-force: a million lbf is 4.45 MN.

03 · Orders of magnitude
FORCE FROM THOUSANDTHS OF A NEWTON TO HEAVY ROCKETS, N, LOGARITHMIC SCALE

04 · Measuring instruments
spring dynamometer
A spring stretches in proportion to the force — Hooke’s law. The scale is in newtons. A school instrument for 1–10 N: an apple is just about one division.
strain gauge · Wheatstone bridge
load cell
Metal under load stretches slightly, and a bonded foil grid changes its resistance. The electronics convert it into newtons. Both scales and firing test stands rely on such sensors.
stand · load cells
static firing stand
The engine is fixed to a frame and fired; the frame presses on load cells. This is how sea-level thrust is measured. Vacuum thrust is obtained in an altitude chamber or calculated from the exit pressure.
a = 3.1 g
accelerometer
An on-board sensor measures the g-load — the force per kilogram of mass. Multiplying it by the current mass gives the thrust minus air drag, right in flight.
05 · Writing rules
Correct
1.9 MN, «1.9 MN» — with a space, capital N
«thrust 1.9 MN at sea level, 2.1 MN in vacuum» — with conditions
«thrust-to-weight ratio 1.4» — no units
1 kgf = 9.80665 N
Incorrect
1.9 mn, 1.9 Mn, 1.9MN — case and space
«200 tonnes of thrust» — a tonne is a mass, thrust is in newtons
«engine thrust 1.9 MN» without altitude — it differs at sea level and in vacuum
«Newton» capitalised in running text — the name is written in lowercase
06 · Neighbouring units
07 · Historical section
throatexit · pₑ · Aₑde Laval nozzle
de Laval nozzle
Metrological note

The newton is a derived SI unit: kilogram, metre and second. Since 2019 the kilogram has been defined through the Planck constant, and the newton rests on it too. Force standards are machines that load a sensor with known weights in a known gravitational field; the largest hold several meganewtons.

The thrust of a rocket engine is not a fixed rating. It depends on the ambient pressure, so specifications give two figures: at sea level and in vacuum. Old handbooks gave thrust in tonnes-force; under GOST 8.417 this is a non-SI unit, converted to newtons by multiplying by 9 807.

Fmg
F greater than mg — liftoff
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