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So Fucking what!
→pf=→procket+→pgas=(m−dmg)(v+dv)^i+dmg(v−u)^i.
pi=pfmv=(m−dmg)(v+dv)+dmg(v−u)mv=mv+mdv−dmgv−dmgdv+dmgv−dmgumdv=dmgdv+dmgv.
The ejection velocity v=2.5×102m/s is constant, and therefore the force is
F=dpdt=vdmgdt=−vdmdt.
With the speed of light ET go home
Honorary Member
Yeah! What @bobcat says
Collins Cp2 map. Ramair induction. Mountune mud flaps. Scorpion Sports Cat. Scorpion Tracker. Wind deflectors. NB washer jets and shark fin aerial. EBC Grooved discs, YellowStuff pads. Airtec Intercooler, Miltek cat back with titanium tips. Collins quickshift. DSC Controller
WHO ARE THESE PEOPLE, 🥴🥴🥴
Eibach Pumaspeed springs UK – Mountune full Induction – delete valve plug – carbon knob – JCR seat lowering kit set @ 39mm – black nuts! Engine forged by FJRS – TCR front splitter V2 and side skirts – RS rallyflapz – Car serviced/maintained by GS Motorsport
Do one. And what Bobcat says.
Coastliner
A spacecraft is moving in gravity-free space along a straight path when its pilot decides to accelerate forward. He turns on the thrusters, and burned fuel is ejected at a constant rate of 2.0×102kg/s, at a speed (relative to the rocket) of 2.5×102m/s. The initial mass of the spacecraft and its unburned fuel is 2.0×104kg, and the thrusters are on for 30 s.
What is the thrust (the force applied to the rocket by the ejected fuel) on the spacecraft?
What is the spacecraft’s acceleration as a function of time?
What are the spacecraft’s accelerations at t = 0, 15, 30, and 35 s?
Strategy
The force on the spacecraft is equal to the rate of change of the momentum of the fuel.
Knowing the force from part (a), we can use Newton’s second law to calculate the consequent acceleration. The key here is that, although the force applied to the spacecraft is constant (the fuel is being ejected at a constant rate), the mass of the spacecraft isn’t; thus, the acceleration caused by the force won’t be constant. We expect to get a function a(t), therefore.
We’ll use the function we obtain in part (b), and just substitute the numbers given. Important: We expect that the acceleration will get larger as time goes on, since the mass being accelerated is continuously decreasing (fuel is being ejected from the rocket).
Solution
The momentum of the ejected fuel gas isp=mgv.
The ejection velocity v=2.5×102m/s is constant, and therefore the force is
F=dpdt=vdmgdt=−vdmdt.
Now, dmgdt is the rate of change of the mass of the fuel; the problem states that this is 2.0×102kg/s. Substituting, we get
F=vdmgdt=(2.5×102ms)(2.0×102kgs)=5×104N.
Above, we defined m to be the combined mass of the empty rocket plus however much unburned fuel it contained: m=mR+mg. From Newton’s second law,a=Fm=FmR+mg.
The force is constant and the empty rocket mass mR is constant, but the fuel mass mg is decreasing at a uniform rate; specifically:
mg=mg(t)=mg0−(dmgdt)t.
This gives us
a(t)=Fmgi−(dmgdt)t=FM−(dmgdt)t.
Notice that, as expected, the acceleration is a function of time. Substituting the given numbers:
a(t)=5×104N2.0×104kg−(2.0×102kgs)t.
At t=0s:a(0s)=5×104N2.0×104kg−(2.0×102kgs)(0s)=2.5ms2.
At t=15s,a(15s)=2.9m/s2.
At t=30s,a(30s)=3.6m/s2.
Acceleration is increasing, as we expected.
Significance
Notice that the acceleration is not constant; as a result, any dynamical quantities must be calculated either using integrals, or (more easily) conservation of total energy.
NOW I APPRECIATE THIS IS A FORD FOCUS RS Mk3 FORUM BUT I THOUGHT I’D SHARE THIS WITH YOU.
PS Sorry if you’re not interested 😹😹😹😹😹😹
Honorary Member
Class 🤣🤣🤣
Eibach Pumaspeed springs UK – Mountune full Induction – delete valve plug – carbon knob – JCR seat lowering kit set @ 39mm – black nuts! Engine forged by FJRS – TCR front splitter V2 and side skirts – RS rallyflapz – Car serviced/maintained by GS Motorsport