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Don't laugh guys, but I'm familiar with a lot of general astronomy stuff but my question will seem very stupid., About rockets, etc.
I was thinking today (dangerous) and realized I don't know the answer to:
Samples: (hypothetical)
1. Space shuttle and all weighs 5 million pounds and total thrust of engines is 6 million pounds, net one million pounds over weight.
2. Payload (any) weighs 500 pounds and thrust in 1,000,500 pounds, net one million pounds over weight.
3. Payload weighs 5 pounds and thrust in 1,000,005 pounds, net one million pounds over weight.
So, not counting air-drag, etc.
Do all three accelerate at the same rate
Do all three reach same velocity in the same amount of time
Would all three reach the same orbit (if programmed the same) at the same time and velocity/altitude
Like I said, dumb question, after midnight, drunk, and I have to pilot an America West flight in 5 hours...:zzz:
I was thinking today (dangerous) and realized I don't know the answer to:
Samples: (hypothetical)
1. Space shuttle and all weighs 5 million pounds and total thrust of engines is 6 million pounds, net one million pounds over weight.
2. Payload (any) weighs 500 pounds and thrust in 1,000,500 pounds, net one million pounds over weight.
3. Payload weighs 5 pounds and thrust in 1,000,005 pounds, net one million pounds over weight.
So, not counting air-drag, etc.
Do all three accelerate at the same rate
Do all three reach same velocity in the same amount of time
Would all three reach the same orbit (if programmed the same) at the same time and velocity/altitude
Like I said, dumb question, after midnight, drunk, and I have to pilot an America West flight in 5 hours...:zzz: