Most Powerful Amateur Rocket in Canada
Alex Schmidt writes "A group of Canadian 'amateur' rocketeers successfully launched a 16 1/2 foot rocket to a height of about 5500 feet. The rocket is based on the 'Dauphine' a meteorological rocket from the 1960's. The rocket weighed 300 pounds, stood 16.5 feet high and 21 inches in diameter. The motors generated 2400lbs of thrust. It successfully landed after 3 of 4 parachutes properly deployed."
I somehow doubt the FAA have jurisdiction for the airspace around, and above Heathrow. That would be the CAA that does, as Heathrow is in the UK, which is not a federal country.
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Andy
You just have to make sure your launch conforms to the following regulations.
Here in er, Canuckistan as I believe some of the Yanks took to calling it, most of us are able to switch effortlessly back and forth between SI and Imperial. For height and weight of things, you'll find typically find we use feet, inches, and pounds (force). You know, people, watermellon, and rockets. Most other measurements use SI. Distance, temperature, viscosity, etc. Mind you, I've never seen vehicles rated by anything other than hp and lb-ft torque. Can you imagine Watts and kN-m?
Project Dauphin website is here.
I believe it's the Saturn V at 3,038,500 kg (I'm not sure how the mass is derived here perhaps with maximum payload and fuel?). The Energia is smaller (2,524,600 kg) with a slightly greater thrust at launch. This meant that the Saturn could lift somewhat more to orbit than the Energia. In comparison, the Shuttle is 2,029,633 kg.
You are aware, I hope, that Canada is involved in NORAD? The North American Aerospace Defense Command. NORAD Quickfacts
>> Anyone know what the largest anywhere was? If you are talking in terms of non-professional rocketry and largest altitude record, I believe it was set by Craig Snyder (US) in 2001. He used a multistage rocket (Type M engines) which reached a very respectable 34,988 ft. You can find most non-professional records here.
Ontario? Grab an Atlas, Calgary is in Alberta.
Nope, wrong again...
According to the specs from Rockets of the World, the SaturnV is as follows;
Stage 1 was 5,800,000,000 N-s, which would make it 5xAC
Stage 2 was 1,200,000,000 N-sec or a 5xAB
Stage 3 was 450,000,000 N-sec or a AC motor
Pardon me if I'm wrong, but I'm noticing a fair amount of "woohoo, I reached 5500 feet with [insert hobby rocket engine here]". However, if you read the article, or think about the Slashdot article, you'll notice that it's not the height that's important, it's the thrust. Most powerful, not highest flying.
I recognize people by their sigs. Is that a bad thing?
According to the project page the total impulse is close to the limit of O class, just under 41,000Ns.
Gee, that article makes it sound like an american invented this (multi-injection orbital gun)... not Gerald Bull.
So howcome it's a "weapon of mass destruction" when Iraq tries to build it, and "space exploration" when an american tries to build it?
Actually, their website says the rocket "featuring a central Cesaroni Pro150 O impulse rocket motor." Also explains why they picked up such a name, Team "O" :-)
Can you imagine Watts and kN-m?
In Australia, vehicles have been rated in kW and kN-M for some years now (10-15 years)
All the car ads in the media mention vehicle specs in metric units. For example, the car (a Holden commodore) I drive has a 156kW buick-derived V6 in it, or you can get a 235kW V8.
Whilst I can convert kW to HP fairly easily in my head, why bother when everything else on the market uses the same units these days?
You are in a twisty maze of processor lines, all alike.
There is a lot of hype here.