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Physics

EOS

Rocket Science

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Stage 2  Saturn V.

no gravity

Stage 2 — The rocket has already jettisoned the Stage 1 frame and has coasted for 4.4 seconds.

vexhaust = 4220 m/s

R = 1190 kg/s

tfinal = 360 s

m0fuel  = 0.428x106 kg

minitial = mfinalStage 1— mjettisonStage 1 = 0.73x106 kg — 0.136x106 kg = 0.594x106 kg

mfinal  = 0.594x106 kg — 0.428x106 kg = .166x106 kg  =  mbody

vinitial for Stage 2 is vfinal of Stage 1—use the Stage 1 result: 3275 m/s—no gravity

**6.5 second coast period between second and third stages;                            displacement given by xcoast = tcoast  vfinal

Stage 2 Results and Graphs — no gravity

Let’s dispense with gravity and look at the results if the Saturn V rocket were to be unfettered.

 

 

webpages and Eos image copyright 2020   M Nealon

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Data for individual stages.

Stage 2  Notes

vfinal 8650 m/s = 19,300 miles/hour

a(tinitial) = .9 g’s

a(tfinal) = 3.1 g’s

x(tfinal) = 1950 km = 1210 miles

After the Stage 2 burn, the rocket jettisons 0.0432x106 kg.

Stage 3  Saturn V.

no gravity

Stage 3 occurs in two burns: the first burn puts the rocket into Earth orbit,

the second is the translunar injection.

Let’s live dangerously and burn it all in one go! . . . why not!*

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Stage 3 Notes

vfinal = 17,100 m/s = 38,200 miles per hour; NASA says the speed at this point would be around 24,500 miles/hour (11,000 m/s).  At this rate the rocket would arrive at the moon in hours, not 3 days!  The reason it takes so long to arrive at the moon is because the rocket slows down.  There’s the influence of gravity again!

a(tfinal) = 5.1 g’s — upwards of 10 g’s becomes painful

x(tfinal) = 3400 miles

Stage 3 Results and Graphs 

Stage 3 — Total burn 477 seconds. 

vexhaust = 4630 m/s

R = 216 kg/s

tfinal = 477 s

m0fuel  = 0.103x106 kg

minitial = mfinalStage 2— mjettisonStage 2 = 0.166x106 kg — 0.0432x106 kg = 0.123x106 kg

mfinal  = 0.123x106 kg — 0.103x106 kg = 0.020x106 kg = mbody

vinitial for Stage 3 is vfinal of Stage 2 — 8650 m/s

*Same results either way.

Page 1

Momentum

Derivation of the Rocket Equation

Thrust

 

Page 2

Speed of the Rocket During the Burn

 

Page 3

Rocket Acceleration

Position as a Function of Time

 

Page 4

Gravity

 

Page 5

Saturn V

Data

Stage 1 Calculation

 

Page 6

Saturn V

Stage 2, Stage 3 Calculations

 

Page 7

Saturn V Photo Gallery

 

Page 8

Saturn V Photo Gallery

 

Page 9

Equation Review

6 —Stage 2 —Stage 3

Stage 2 equations – no gravity

Stage 3 equations – no gravity

minitial

(x10kg)

mfinal

(x106 kg)

vinitial

(m/s)

vfinal

(m/s)

a(t=0)

(m/s2)

a(tfinal)

(m/s2)

x(tfinal)

(km)

xcoast**

(km)

Final

Altitude

(km)

0.594

.166

3275

8650

8.45

30.2

1950.

56.2

2010.

 

 

 

 

 

 

 

 

 

 

m0fuel

Fuel

Mass

(x106kg)

T

Thrust

(x106N)

tfinal

Burn Duration

(s)

vexhaust

Exhaust Velocity

(m/s)

R

Burn Rate

(kg/s)

Frame Mass to jettison

(X106kg)

First stage

2.04

33.4

150

2456

13600

0.136

Second stage

.428

5.02

360

4220

1190.

0.0432

Third stage

a

0.0356

1.00

165

4630

216.

— not yet

b

0.0674

1.00

312

4630

216.

0.0174

minitial

(x10kg)

mfinal

(x106 kg)

vinitial

(m/s)

vfinal

(m/s)

a(t=0)

(m/s2)

a(tfinal)

(m/s2)

x(tfinal)

(km)

Xcoast

(km)

Final

Displacement

(km)

 

0.123

 

0.020

8650

 

17,100

 

8.1

 

50.

 

5,560

all the way to the moon

 

5,560

 

 

 

 

 

 

 

 

 

 

m0fuel

Fuel

Mass

(x106kg)

T

Thrust

(x106N)

tfinal

Burn Duration

(s)

vexhaust

Exhaust Velocity

(m/s)

R

Burn Rate

(kg/s)

Frame Mass to jettison

(X106kg)

Third stage

a

0.0356

1.00

165

4630

216.

— not yet

b

0.0674

1.00

312

4630

216.

0.0174

Third stage in one burn

0.103

1.00

477

4630

216.

0.0174