Intuition The one core idea
A flying rocket is just an arrow (its velocity) that lives at a moving point. To predict the whole flight we only ever ask two questions about that arrow: is it getting longer or shorter (speed), and which way is it turning (direction) — plus where its tip has travelled. Every symbol in the parent note is a name for one piece of that arrow-tracking story.
This page assumes you have seen none of the notation on the parent page. We build each symbol from a picture, in an order where each one only needs the ones before it. By the end you can read the parent equations left to right without ever meeting an unexplained mark.
Everything happens in a flat vertical plane: a floor (the ground) and a wall (straight up). We watch one dot — the rocket, shrunk to a point — move across this plane.
A point mass is an object shrunk to a single dot that carries all its mass but has no size and no orientation . It can be somewhere and it can move , but it cannot spin — a dot has no "which way am I facing."
Picture: the red dot in the figure. Why we need it: the whole topic ("3DOF") is the claim that for finding a trajectory, this dot is all the rocket we need.
To say where the dot is, we need two numbers, because the plane is two-dimensional.
x — downrange distance, h — altitude
x = how far the dot has travelled along the ground (horizontal), measured from the launch point. Picture: the shadow of the dot on the floor.
h = how high the dot is above the ground (vertical). Picture: the height of the dot above its shadow.
Together ( x , h ) is the dot's address in the plane.
Why the topic needs them: the final product of a trajectory analysis is a curve of h against x — the flight path drawn on the wall. Everything else exists to compute how ( x , h ) changes.
The dot moves, so it has a velocity — an arrow whose length is the speed and whose direction is where it's heading. Instead of splitting velocity into "horizontal part" and "vertical part," the parent note describes the arrow directly with its length and its tilt . This is the single most important idea to get comfortable with.
V — speed (length of the velocity arrow)
V is how fast the dot moves, in metres per second (m/s ). It is the length of the velocity arrow — always a positive number (or zero). It says nothing about direction.
γ — flight-path angle (tilt of the velocity arrow)
γ (the Greek letter gamma ) is the angle the velocity arrow makes above the horizontal . Picture: start from the floor-direction and swing up to the arrow — that opening is γ .
γ = 0 → flying flat (horizontal).
γ = 9 0 ∘ → flying straight up.
γ < 0 → nose pointing below horizontal (falling / descending).
Intuition Why length-and-tilt instead of horizontal-and-vertical?
Newton's law changes a vector . A vector has exactly two properties: magnitude and direction . If we track those two directly (V and γ ), then "engine pushes forward" changes only V , and "gravity pulls sideways to the arrow" changes only γ . The physics falls apart into two clean, separate stories. That is the entire reason this frame is used.
The symbols sin γ and cos γ appear everywhere in the parent note. Here is what they are , from zero.
Drop the velocity arrow into a right triangle: its horizontal shadow, its vertical rise, and the arrow itself as the slanted side (the hypotenuse , length V ).
Definition Sine and cosine of the flight-path angle
For the right triangle built on the velocity arrow (hypotenuse length V , angle γ at the origin):
cos γ = hypotenuse horizontal side = V along-ground part → so the horizontal part of velocity is V cos γ .
sin γ = hypotenuse vertical side = V up part → so the vertical part of velocity is V sin γ .
Why these two tools and not others? Sine and cosine are the only functions that convert an angle-plus-length into its horizontal and vertical pieces. Any time you must split a slanted arrow into flat and upright parts, these are the machines that do it. That is exactly the job here.
Common mistake Which one is which?
The fix — anchor to the extremes. At γ = 9 0 ∘ (straight up) the whole arrow is vertical: the up-part must equal V . Since sin 9 0 ∘ = 1 , the vertical part is sin γ . At γ = 0 (flat) the whole arrow is horizontal: cos 0 = 1 gives the horizontal part cos γ . Test the extreme and you never mix them up.
This immediately explains two boxed kinematic equations from the parent:
x ˙ = V cos γ ( horizontal part ) , h ˙ = V sin γ ( vertical part ) .
The parent note is full of symbols wearing a dot on top. This is not decoration.
Definition The overdot — "rate of change per second"
A dot over any quantity means "how fast that quantity is changing, per second ."
V ˙ = how fast the speed is changing = acceleration along the arrow (m/s 2 ).
γ ˙ = how fast the tilt is changing = how quickly the arrow is turning (rad/s ).
x ˙ , h ˙ = how fast the address changes = the velocity's horizontal and vertical parts.
m ˙ = how fast the mass is changing (negative — fuel is leaving).
Intuition Why we care about rates, not values
We rarely know exactly where the rocket will be. But at any instant we can write down the forces, and forces tell us rates of change . So the natural language is: "given the state now, here is how fast each thing is changing." Feed those rates forward moment by moment and the whole flight path unrolls. (Doing that feed-forward is the job of Numerical Integration of Trajectories (RK4) .)
An equation with a dotted variable on the left ("V ˙ = … ") is called an ODE — an equation for a rate . The parent's four boxed equations are four such rate-rules.
The rate of the arrow's length and tilt is set by forces . Four of them, each with its own symbol.
Definition The force symbols
m = mass (kilograms): how much stuff must be pushed. Bigger m → harder to speed up.
g = gravitational acceleration (≈ 9.81 m/s 2 ): how hard gravity pulls each kilogram down.
m g = weight : the total downward pull (mass × g ). Always points straight down.
T = thrust : the engine's push, pointing along the velocity arrow (forward).
D = drag : air resistance, pointing backward along the arrow (always opposes motion).
L = lift : a force perpendicular to the arrow (often 0 for a symmetric rocket).
Definition The drag formula's symbols
Drag is D = 2 1 ρ V 2 S C D , where:
ρ (Greek rho ) = air density — how thick the air is (thins out with altitude).
S = reference area of the vehicle (how much air it shoves aside).
C D = drag coefficient — a shape-and-speed number for how "draggy" the body is.
V 2 = speed squared: doubling speed quadruples drag.
You don't derive this here — Drag and Atmospheric Models supplies it. You only need to know D is a backward push whose symbol is D .
Intuition Why weight splits with sine and cosine
Thrust and drag already lie along the arrow — easy. But weight points straight down , not along the arrow. To use it in the length-and-tilt story we must split it into an along-arrow part and an across-arrow part — exactly the sine/cosine job from Section 3. Geometry gives:
along the arrow (opposing climb): m g sin γ → shrinks V .
across the arrow (bending the path down): m g cos γ → makes γ ˙ negative.
This is the whole content of the parent's "S-along, C-across " mnemonic.
In the mass-rate rule m ˙ = − T / ( I s p g 0 ) two new symbols appear.
I s p and g 0
I s p = specific impulse — an efficiency rating for the engine: how much "push-seconds" you get per unit of propellant weight. Higher I s p → you burn fuel more slowly for the same thrust.
g 0 = 9.80665 m/s 2 — a fixed reference value of gravity used only to define I s p 's units. It is a constant, not the local gravity g .
Why the topic needs them: they turn "how much thrust" into "how fast fuel disappears," which is what makes m shrink over time. The deep consequences of shrinking mass are the story of the Tsiolkovsky Rocket Equation .
Flight-path angle gamma - arrow tilt
Sine and cosine - split the arrow
Overdot - rate per second
Mass rate with Isp and g0
Read it as: the dot gives us position and velocity; velocity gives length (V ) and tilt (γ ); trig splits the arrow; forces split by trig set the rates; all rates together are the 3DOF equations. See also Flight-Path Angle and Velocity Frame for the geometry of γ , and 6DOF Rigid-Body Dynamics for what we deliberately left out.
Cover the answers and test yourself before opening the parent note.
What does a "point mass" keep, and what does it throw away? Keeps mass and position/motion; throws away size and orientation (it cannot spin).
What two numbers describe the velocity arrow in this frame? Its length V (speed) and its tilt γ (flight-path angle).
The vertical part of velocity is V times which trig function? sin γ — check with γ = 9 0 ∘ : all velocity is vertical and sin 9 0 ∘ = 1 .
The horizontal part of velocity is V times which trig function? cos γ — check with γ = 0 : all velocity is horizontal and cos 0 = 1 .
What does the dot in V ˙ mean? The rate of change of V per second (here, acceleration along the arrow).
Which way does drag D point? Backward, directly opposing the velocity arrow.
Weight points straight down — into what two pieces do we split it? Along the arrow m g sin γ (slows climb) and across it m g cos γ (turns the path).
What is g 0 and how does it differ from g ? A fixed constant 9.80665 m/s 2 used to define I s p ; g is the actual local gravity.
Why do we track rates of change instead of positions directly? Forces tell us rates; feeding rates forward moment by moment reconstructs the whole path.