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Momentum Keeps No Memory of Launch

Irodov 1.96DifficultyDifficulty 2 of 5UniquenessUniqueness 3 of 5

Problem Irodov 1.96

A body of mass mm is launched with initial velocity v0\vect v_0 at some angle to the horizontal and moves freely under constant gravitational acceleration g\vect g, air resistance neglected. Find:

  1. the momentum increment Δp\Delta\vect p acquired over the first tt seconds of the flight

  2. the magnitude of the momentum increment Δp\Delta\vect p over the whole flight, from launch until the body returns to its launch height

The free flight the problem describes. The body leaves O with the given velocity v_0 and passes a later point P of the path, where its velocity is v(t), still tangent to the path.

The free flight the problem describes. The body leaves OO with the given velocity v0\vect v_0 and passes a later point PP of the path, where its velocity is v(t)\vect v(t), still tangent to the path.

Given
  • mm
  • v0\vect v_0
  • g\vect g
Find
(a) Δp\Delta\vect p over the first tt seconds, (b) ∣Δp∣|\Delta\vect p| over the whole flight

Solution

Step 1Part (a): the impulse of gravity over [0,t][0,t]

With air drag neglected, gravity is the only force on the body, so the momentum increment is the impulse of mgm\vect g, constant, integrated over the elapsed time.

Δp(t)=∫0tmg dτ\Delta\vect p(t) = \int_0^t m\vect g\,d\tau
Δp(t)=mg t\Delta\vect p(t) = m\vect g\,t
(1)
The velocity triangle at P: a ghost copy of v_0 (dashed) carried across to P sits tail to tail with v(t), and the third side, joining their tips, is g t pointing straight down.

The velocity triangle at PP: a ghost copy of v0\vect v_0 (dashed) carried across to PP sits tail to tail with v(t)\vect v(t), and the third side, joining their tips, is g t\vect g\,t pointing straight down.

Step 2The displacement, for the landing condition

Part (b) needs the total flight time TT, which requires the displacement. Dividing (1) by mm gives v(t)=v0+gt\vect v(t) = \vect v_0+\vect g t, and integrating that once more gives the displacement.

r(t)=∫0t(v0+gτ) dτ=v0t+gt22.(2) \vect r(t) = \int_0^t\bigl(\vect v_0+\vect g\tau\bigr)\,d\tau = \vect v_0 t+\frac{\vect g t^2}{2}. \tag{2}
Step 3The total flight time

The flight ends at the instant TT when the body returns to launch height, so the displacement then has zero component along g\vect g. Dotting the displacement (2) with g\vect g and keeping the nonzero root isolates TT.

0=r(T)⋅g=T(v0⋅g)+T2g22=T[(v0⋅g)+Tg22]\begin{align*}0 &= \vect r(T)\cdot\vect g \\ &= T(\vect v_0\cdot\vect g)+\frac{T^2g^2}{2} \\ &= T\left[(\vect v_0\cdot\vect g)+\frac{Tg^2}{2}\right]\end{align*}

T=0T=0 is the launch instant itself; the flight time is the other root, where the bracket vanishes.

T=−2(v0⋅g)g2T = -\dfrac{2(\vect v_0\cdot\vect g)}{g^2}
(3)
Step 4Part (b): the momentum increment over the whole flight

The increment (1) holds for any elapsed time, so setting t=Tt=T and substituting (3) gives the momentum increment over the whole flight; its magnitude is mgmg times TT, since g T\vect g\,T and g\vect g share a direction.

∣Δp(T)∣=mg T=mg(−2(v0⋅g)g2)\begin{align*}\left|\Delta\vect p(T)\right| &= mg\,T \\ &= mg\left(-\frac{2(\vect v_0\cdot\vect g)}{g^2}\right)\end{align*}
∣Δp∣=−2m(v0⋅g)g\left|\Delta\vect p\right| = -\dfrac{2m(\vect v_0\cdot\vect g)}{g}
(4)
Check

Dimensionally [m(v0⋅g)/g]=kg⋅(m/s)(m/s2)/(m/s2)=kg⋅m/s[m(\vect v_0\cdot\vect g)/g] = \text{kg}\cdot(\text{m/s})(\text{m/s}^2)/(\text{m/s}^2) = \text{kg}\cdot\text{m/s}, a momentum. The minus sign is necessary rather than decorative: v0\vect v_0 has a component against g\vect g at launch, so v0⋅g<0\vect v_0\cdot\vect g<0 and the whole expression comes out positive, as a magnitude must. For a body launched exactly horizontally (v0⋅g=0\vect v_0\cdot\vect g=0), T=0T=0: it never rises above its launch height at all, so there is no later instant at which to measure a nonzero return.

Remark

Part (a)’s result carries no memory of the launch: Δp(t)=mg t\Delta\vect p(t)=m\vect g\,t depends only on the elapsed time, never on v0\vect v_0, because gravity’s impulse rate dp/dt=mgd\vect p/dt=m\vect g is the same at every instant of every trajectory under this constant field. The initial velocity only ever enters through TT in part (b), which sets how long the flight lasts, not the rate at which momentum is changing during it.