• Want to help us with this year's BoS Trials?
    Let us know before 30 June. See this thread for details
  • Looking for HSC notes and resources?
    Check out our Notes & Resources page

Help with a Space question? (1 Viewer)

Aluminesis

Member
Joined
Nov 8, 2009
Messages
54
Gender
Female
HSC
2011
Hey guys, I'm doing past half-yearly papers and I got stumped on a question. Hoping I can get some help here.

Question:
[FONT=&quot]In the launch of a particular satellite, the satellite was release from a rocket such that it moved into a stable orbit around the Earth. After the satellite had completed a number of orbits of Earth, each taking 90 minutes, onboard rockets were used to propel the satellite into a much more distant stable orbit, with a radius 10 times larger than the original. Based on this information, which of the following could be closest to the orbital period of the satellite in the final more distant orbit?[/FONT]
[FONT=&quot] [/FONT]
[FONT=&quot](A) 47.4 hours[/FONT]
[FONT=&quot](B) 38.7 hours [/FONT]
[FONT=&quot](C) 22.5 hours [/FONT]
[FONT=&quot](D) 15 hours [/FONT]

The answer is A. I tried using Kepler's Law of Periods but it didn't work out. Am I approaching it from the wrong angle or am I on the right track but making silly mistakes?

I'd really appreciate it if someone could post the full working out involved with this question. Thanks!
 

laplace4

Banned
Joined
Mar 28, 2011
Messages
6
Gender
Undisclosed
HSC
N/A
That is so easy, you might as well just give up on hsc altogether if you cant do that
 

Aluminesis

Member
Joined
Nov 8, 2009
Messages
54
Gender
Female
HSC
2011
I'm sure it is, mate, but not every person who can't tie their shoelace goes and chucks their shoe out the window so I'll take my chances
 

laplace4

Banned
Joined
Mar 28, 2011
Messages
6
Gender
Undisclosed
HSC
N/A
nah you are a no hoper lol

use the keplar eqn to find the initial distance from the centre of the earth, then multiply that value by 10, then sub that back ito the eqn and solve the period

there are only two unknowns in the equation , r and T , if you know one you can find the other
 

OmmU

★ BoS Deity ★
Joined
Jan 21, 2011
Messages
404
Location
Middleofnowhere
Gender
Male
HSC
2011
Uni Grad
2017
Answer is A.

I suspect you are having some calculation errors:

My working:

Find out the initial orbital radius:

Plug your info into the formula:


Rearrange and don't forget to cube root to get r. (Since only goes to like 4dp, wrote down to 4dp.

Then plug 10r into the equation and rearrange to get :




= 47.4hrs
 

laplace4

Banned
Joined
Mar 28, 2011
Messages
6
Gender
Undisclosed
HSC
N/A
lol you are a noob too, you didnt even need constants to do it
 

laplace10

Banned
Joined
Mar 29, 2011
Messages
5
Gender
Female
HSC
N/A
lol you dont even need the constants or anything

you can just simplify everything down to final period = sqrt ( 10^3 x T^2 ) , where T is the first period.

Thats just by pure algberaic manipulation
 

Fizzy_Cyst

Well-Known Member
Joined
Jan 14, 2011
Messages
1,189
Location
Parramatta, NSW
Gender
Male
HSC
2001
Uni Grad
2005
Hey guys, I'm doing past half-yearly papers and I got stumped on a question. Hoping I can get some help here.

Question:
[FONT=&quot]In the launch of a particular satellite, the satellite was release from a rocket such that it moved into a stable orbit around the Earth. After the satellite had completed a number of orbits of Earth, each taking 90 minutes, onboard rockets were used to propel the satellite into a much more distant stable orbit, with a radius 10 times larger than the original. Based on this information, which of the following could be closest to the orbital period of the satellite in the final more distant orbit?[/FONT]
[FONT=&quot] [/FONT]
[FONT=&quot](A) 47.4 hours[/FONT]
[FONT=&quot](B) 38.7 hours [/FONT]
[FONT=&quot](C) 22.5 hours [/FONT]
[FONT=&quot](D) 15 hours [/FONT]

The answer is A. I tried using Kepler's Law of Periods but it didn't work out. Am I approaching it from the wrong angle or am I on the right track but making silly mistakes?

I'd really appreciate it if someone could post the full working out involved with this question. Thanks!
Seeing as it is still orbiting around the same object r^3/T^2 is constant.

T^2 final = (r^3final * T^2 initial)/r^3 initial


T^2 final = (r^3final/r^3 initial) * T^2 initial

T^2 final = (r final / r initial)^3 * T^2 initial

T^2 final = (10)^3 * 90^2

T final = sqrt (1000*8100)

T final = 2846mins

T final = 47.43hrs
 

jyu

Member
Joined
Nov 14, 2005
Messages
623
Gender
Male
HSC
2006
Seeing as it is still orbiting around the same object r^3/T^2 is constant.

T^2 final = (r^3final * T^2 initial)/r^3 initial


T^2 final = (r^3final/r^3 initial) * T^2 initial

T^2 final = (r final / r initial)^3 * T^2 initial

T^2 final = (10)^3 * 90^2

T final = sqrt (1000*8100)

T final = 2846mins

T final = 47.43hrs
wording of the question
10 times longer than the original means 11 times the original?
 

Fizzy_Cyst

Well-Known Member
Joined
Jan 14, 2011
Messages
1,189
Location
Parramatta, NSW
Gender
Male
HSC
2001
Uni Grad
2005
True, that could definitely be debated!

But then the answer would be greater than 47.43, prolly closer to 55. Seeing as that is not an option in the answers, the answer must be 47.43 =)
 

Users Who Are Viewing This Thread (Users: 0, Guests: 1)

Top