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Author
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Topic: Phi = God?
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SRO2 
Inactive Member
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Message 5 of 20 (97659)
04-04-2004 10:34 AM
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Reply to: Message 4 by RAZD
04-03-2004 11:55 PM
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Re: (1+5e-2)/2
I'm a be-leever.
| This message is a reply to: | | | Message 4 by RAZD, posted 04-03-2004 11:55 PM | | RAZD has replied |
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SRO2
Inactive Member
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Message 7 of 20 (97753)
04-04-2004 11:07 PM
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Reply to: Message 6 by RAZD
04-04-2004 12:46 PM
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Re: (1+5e-2)/2
Well, I'm glad you asked that Mr. Leever. Yes, indirectly, it's one of the most critical equations in rocket science. It typically expressed as the nozzle exit plane ratio to the thrust chamber diameter...maximum efficiency at sea-level AND in a vacuum....both are in terms of diameter, but neither have a darn thing to do with tree rings, elbows or the "impoverishly rounded objects" that rockets are designed to travel to.
| This message is a reply to: | | | Message 6 by RAZD, posted 04-04-2004 12:46 PM | | RAZD has replied |
| Replies to this message: | | | Message 8 by RAZD, posted 04-05-2004 12:00 AM | | SRO2 has replied |
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SRO2
Inactive Member
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Message 9 of 20 (97765)
04-05-2004 12:06 AM
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Reply to: Message 8 by RAZD
04-05-2004 12:00 AM
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Re: (1+5e-2)/2
It is, along with weight...MDOT is how you derive ISP (Specific impulse) required for a given mass for a given distance at optimum efficiency (gas mileage (they hate it when I call it that).
| This message is a reply to: | | | Message 8 by RAZD, posted 04-05-2004 12:00 AM | | RAZD has not replied |
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SRO2
Inactive Member
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Re: Abby Leever= Rocket retriever
No. I promise I'm not. I have a website but I can't give out the address. If Abby wants to e-mail you the address he can, it has seperate photos of he and I. It's up to Abby if he wants to give it to you if you really need proof.
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SRO2
Inactive Member
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Re: Abby Leever= Rocket retriever
HEY! DID YOU JUST SHOOT ME A BIRD!?!
| This message is a reply to: | | | Message 13 by mike the wiz, posted 04-13-2004 9:12 PM | | mike the wiz has not replied |
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