Wednesday, May 22, 2013
TR-1 MOTOR UPDATE
GROVER AEROSPACE
I went though my links to see what other people were doing. Some are less active than they use to be, some more. I got rid of a couple of links and I also found some new sites. One that I found to be particularly interesting is James Grover's site. I hadn't read very far before I found this sentence that he had written in the response to a question. "I don't have a lathe so I "turned" the parts with a hand drill and made the o-ring grooves with a hack saw blade." To me that sentence exemplifies the can do spirit of a true amateur experimental rocketeer. Anyway, lots of interesting stuff on his site and worth checking out.
Tuesday, May 21, 2013
TR-1 MOTOR UPDATE
Monday, May 20, 2013
TR-1 MOTOR UPDATE
I may still decide to take some excess weight out of the nozzle ring as it's heavier than it needs to be. Then again, it doesn't really matter for the static test so I may just get the important stuff done then move onto the next piece. It would be beneficial to remove weight from the aft end of the rocket before the flight so I'm sure I'll do it before then. I'm machining the nozzle ring out of 1018 which is noticeably tougher to machine than the 12L14 that I'll be using for the divergent piece. Once you've machined 12L14 steel, all other steel seems like a chore!
Labels:
machining,
nozzle,
rocket nozzle,
TR-1 Rocket
Friday, May 17, 2013
TR-1 MOTOR UPDATE
I started on the nozzle ring this morning. I drilled out the center, starting with a center bit and working up to a 1" diameter bit. The larger drill bits remove a lot of material quickly, but an inch is about the limit for my lathe. Next I'll bore out the center to the right diameter. Then I'll face it, cut the relief that the divergent section fits into, and index the holes for the six screws that hold the two sections together. Then I'll flip the piece. Once flipped I can finish it off to the correct diameter and cut the convergent section. Lastly I'll add the o-ring gland and index the twelve screw locations for the screws that hold it in the casing.
Thursday, May 16, 2013
SStS MOTOR CASING (DSS TM-3)
The aluminum tube for the DSS-TM-3 SStS motor arrived yesterday. I'm just indexing/drilling the screw holes so not much work for me. DSS TM-3 motor? OK, it's getting tough to keep track of all the motors as there are more than a few in varies stages of construction and testing. The motor is a single burn (half of the dual phase concept) that is intended to serve as a flight motor for the avionics package once successfully tested. The design calls for approximately 90 lbs (41 Kg) of propellant. Hopefully that flight will occur later this year. As always, check the weekly reports on the Sugar shot to Space site for more detailed information.
CHARLES M. PARKIN, JR.
Charles M. Parkin, Jr. as he is described in the book:
Rocket expert, U.S. Army Engineer, Research and Development Laboratories, Fort Belvoir, Virginia; Founder of Youth Science Corps; President, American Rocket Society, Washington D.C. chapter.
In the later chapters of the book, he describes a small rocket which utilizes a sugar based propellant. I've often thought that it would be fun to build that rocket exactly to the specification in the book and then actually fly it.
Maybe I will do that some day...
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