India does not have an ICBM programme

[Kinetic]

No your statement is very confusing to the public. It's better to make things clear before progressing.

If you don't understand the meaning of a post and bring 8th grade physics to prove simple thing and than troll, what can one do?

What did you got from this post? Do you got anything more than orbit? Is this post has anything to do with orbit?

"You are just pretending not to understand something which is very clear! Indian rocket reaches the Moon which is 384,403 kilometres away from the Earth. We put satellites into Geosynchronous orbit which is 36000 km away. Our Agni-III can carry 2500 kg payloads to 3500 km away. Now every people with little common sense will understand that whether India can build ICBM or not. If you say, 'I will never believe that', thats something upto you."

 

[lhuang]

No your statement is very confusing to the public. It's better to make things clear before progressing.

For the record, there are Indians in the Chinese threads posting flame comments with the Chinese not commenting "Troll troll troll" to every flame post made. Why are you over reacting so much?

I think we have all deviated from the original topic.

But these kind of threads should be encouraged, this is the first forum I have signed up on, but I have only seen such discussions on Bharat-Rakshak forums. But I don't think there are any Chinese on that forum, so I am here and I am here to learn.

 

[lockh33d]

What you say is correct, but the altitude of GSO from earth's surface is 35786 km.

GTO is an intermediate orbit which is reached for the satellite to be put in the GSO.

Read post #116 again. Mathematically speaking, what you say in incorrect.

 

[lockh33d]

If you don't understand the meaning of a post and bring 8th grade physics to prove simple think and than troll, what can one do?

What did you got from this post? Do you got anything more than orbit? Is this post has anything to do with orbit?

"You are just pretending not to understand something which is very clear! Indian rocket reaches the Moon which is 384,403 kilometres away from the Earth. We put satellites into Geosynchronous orbit which is 36000 km away. Our Agni-III can carry 2500 kg payloads to 3500 km away. Now every people with little common sense will understand that whether India can build ICBM or not. If you say, 'I will never believe that', thats something upto you."

384,403 kilometres away from the Earth's SURFACE.

We put satellites into Geosynchronous orbit which is 36000 km away from the surface of our planet.

 

[jha]

The highlighted part is incorrect.

You are equating GSO and GTO.

GSO is a perfect circular orbit while GTO is a highly elliptical orbit.

yes very true....without taking a pause and thinking everybody seems to be gung-ho.

A circular geosynchronous orbit in the plane of the Earth's equator has a radius of approximately 42,164 km (26,199 mi)(from the center of the Earth). A satellite in such an orbit is at an altitude of approximately 35,786 km (22,236 mi) above mean sea level.


A geosynchronous transfer orbit or geostationary transfer orbit (GTO) is an intermediate orbit used to reach geosynchronous or geostationary orbit.[1] It is a highly elliptical Earth orbit with apogee at about 35,700 km, geostationary (GEO) altitude, and an argument of perigee such that apogee occurs on or near the equator. Perigee can be anywhere above the atmosphere, but is usually limited to only a few hundred km.

 

[jha]

I think we have all deviated from the original topic.

But these kind of threads should be encouraged, this is the first forum I have signed up on, but I have only seen such discussions on Bharat-Rakshak forums. But I don't think there are any Chinese on that forum, so I am here and I am here to learn.

this is the first good thing about bharat rakshak i have heard from a non-indian...the posts there might be indian but contain a deep down analysis of the core..

 

[lockh33d]

yes very true....without taking a pause and thinking everybody seems to be gung-ho.

A circular geosynchronous orbit in the plane of the Earth's equator has a radius of approximately 42,164 km (26,199 mi)(from the center of the Earth). A satellite in such an orbit is at an altitude of approximately 35,786 km (22,236 mi) above mean sea level.


A geosynchronous transfer orbit or geostationary transfer orbit (GTO) is an intermediate orbit used to reach geosynchronous or geostationary orbit.[1] It is a highly elliptical Earth orbit with apogee at about 35,700 km, geostationary (GEO) altitude, and an argument of perigee such that apogee occurs on or near the equator. Perigee can be anywhere above the atmosphere, but is usually limited to only a few hundred km.

One question, how can something be elliptical if you have a CONSTANT 35,700 above the surface? That would surely make it circular wouldn't it? Just a thought...

 

[jagjitnatt]

Read post #37 again. Mathematically speaking, what you say in incorrect.

Actually what you countered in the first place was not required because there was nothing wrong with his statement that GSO is 36k from surface of earth.

I at first got confused about what you were trying to say and didn't have much idea of how much physics you could grasp, hence that simplified response.

 

[Kinetic]

384,403 kilometres away from the Earth's SURFACE.

We put satellites into Geosynchronous orbit which is 36000 km away from the surface of our planet.

The Moon is 384403 km away from the Earth and Geo orbit is 36000 km away. But that was not the meaning of that post. you got it wrong.

 

[lockh33d]

OK, I think I proved my point a while ago, so it's time for me to hit the hay. Good night fellas.

 

[jha]

One question, how can something be elliptical if you have a CONSTANT 35,700 above the surface? That would surely make it circular wouldn't it? Just a thought...

my god..some body here can give a lesson on CO-ordiante geometry..??
i cant because i am going now...

GTO is ELLIPTICAL with APOGEE and PERIGEE>>

APOGEE-35700 km.

 

[jagjitnatt]

One question, how can something be elliptical if you have a CONSTANT 35,700 above the surface? That would surely make it circular wouldn't it? Just a thought...

GTO is not constant. It is highly elliptical. It is not a fixed radius shape. It is just an intermediate orbit. This is where we intent to catapult the satellite. Any object projected at this orbit would automatically go into GSO.

Let me find some images. That would make it a lot easier. Can't describe it in words.

 

[jagjitnatt]

This is a good example of GTO, where a satellite eventually goes into GSO

 

[jagjitnatt]

GTO and GSO perfectly visible here.

 

[ARCHON]

The Moon is 384403 km away from the Earth and Geo orbit is 36000 km away. But that was not the meaning of that post. you got it wrong.

Forgive him he didnt fully read the post and the link he got from sudden googling..