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Blackwell 1


Cody Blackwell

Mrs. Corbett

AP English Lit/Comp

18 April 2012

                                        High-Power Rocketry

       “Research is what I am doing when I don’t know what I’m doing.” It may surprise you

that I began this presentation with that statement, but I am only repeating a quote from our

nation’s most celebrated rocket scientist, Dr. Wernher von Braun. Through the Army Ballistic

Missile Agency (ABMA), Dr. von Braun and an extremely bright team of engineers and

researchers revolutionized America’s defense and space exploration technology as we know

them. ABMA’s research proved most instrumental to NASA’s Apollo program, but, as with any

substantial scientific strides, the program had its flaws. More specifically, my research paper

discusses the events leading up to Apollo XIII and how Jim Lovell, Fred Haise, and Jack Swigert

survived for nearly six days after two oxygen tank explosions in the command module. I plan to

study aerospace engineering, and in keeping with the problem-solving spirit, I focused on the

ingenious valve NASA engineers developed from duct tape, plastic bags, and cardboard that

supplied the three astronauts enough oxygen to return safely home.

       One might ask, “How can Apollo XIII possibly relate to high-power rocketry?” When I

first received instructions for this project, I considered researching techniques for integrating

gravity-fed cooling systems into nuclear plants in the wake of the Fukushima Daiichi disaster but

ruled it out after assessing its practicality. Building on this practicality, I realized it made much

more sense if I built on my prior experiences, namely in amateur rocketry. I have been a member

of Creekview Aeronautics Club for the past four years, and our teams have only used relatively
Blackwell 2


low-impulse engines in our rockets for Team America Rocketry Challenge. High-power rocketry

(HPR), on the other hand, is an entirely different ball game, and I chose to build and launch a

high-power rocket specifically because it requires meticulousness and considerably more time

than anything the Aeronautics Club does. Accordingly, I encountered an issue I will discuss

momentarily which presented an almost project-ending conundrum requiring me, like Mission

Control, to work with what little supplies I had.

       As I learned from members of Southern Area Rocketry (SoAR)—our local National

Association of Rocketry (NAR) chapter—and namely Mr. Todd Sharrock and Coach Tim Smyrl,

a HPR certification is a prized possession among hobbyists and university clubs. For example,

NAR Level I certification (my goal) authorizes flight privileges for rockets weighing over 53

ounces (3.3 pounds), with total impulses between 160.01 Newton-seconds and 640 Newton-

seconds, and/or engines not classified as “model rocket motors.” I figured if I could push myself

to achieve Eagle Rank, building and flying a high-power rocket for said authorization would be

no problem. But like the trail to Eagle, this project required a dedicated mentor, an accountability

coach who would scrutinize any changes I made before approving them. As a charter member of

the Aeronautics Club and a team captain for the past three years, I know both Mr. Sharrock and

Coach Smyrl well. However, I selected Mr. Sharrock because he taught my freshman biology

course and our lunch periods happened to coincide this year. Over the past seven months, we

met regularly to discuss design options, component suppliers, and any problems I encountered

along the way.

       Consequently, the essence of engineering commands careful consideration and

consultation before any project commences. For several days in December, Mr. Sharrock and I

discussed his and Coach Smyrl’s successful Level I designs as well as reliable component
Blackwell 3


vendors. Finally settling on Public Missiles Limited (PML), I began designing my rocket using

Apogee Components’ RockSim 9.0 software, basing the prototype off a PML parts list in the

software’s database. I simultaneously researched high-power rocket plans and stumbled across a

recovery system I had never seen.

       Since the Aeronautics Club’s inception, we have attached one parachute each to our

rockets’ payload and airframe sections, allowing the two to return separately to the ground.

However, the system I found and eventually utilized is a single-chute design using a piston that

eliminates the need for a black-powder ejection charge. This system allows for the parachute to

be linked with the piston and nosecone by a shock cord and stored without any wadding between

the piston and the nosecone; the reloadable motor’s delay forces the piston, parachute, and

nosecone out of the tube, keeping all parts of the rocket together during its descent. The only

flaw was that I could not use a launch rail system like Mr. Sharrock’s rocket because the guide

pins would obstruct the piston. Regardless, I showed Mr. Sharrock and Coach Smyrl, who both

heartily recommended it because they have never tried it themselves. Regarding the rest of the

rocket, I incorporated the same motor mount design we use in Aeronautics Club with the

exception of the motor retainer, which NAR strongly encourages hobbyists to use for high-power

rockets, and the number of fins (three instead of four). I settled on slotted phenolic tubing, a

hardened parabolic nose cone, and fiberglass fins so, as Mr. Sharrock pointed out, I would at

least have something to show in case of a catastrophic failure!

       Thankfully, all of the parts shipped together over Christmas break. Around that time, I

also researched the different types of reloadable motors supplied by AeroTech Consumer

Aerospace and Cesaroni Technology, Inc. Again, my membership in the Aeronautics Club

exposed me to AeroTech reloadable motors; however, our brand new reloads were not
Blackwell 4


performing well at the time, and Cesaroni seemed to offer a much higher-quality lineup of 29

mm-diameter motors for substantially lower prices. Using RockSim-generated flight predictions

for comparable motors and data sheets provided by AeroTech and Cesaroni, I determined the

Cesaroni H87-12A, with an average thrust of 87 Newtons and a 12 second delay, was most

suitable for my certification purposes.

        Assembling the rocket did not prove too difficult, thanks to my prior experiences, and I

started from the bottom up. The motor mount consisted of two customary plywood centering

rings, one of which had a slot cut into it so I could glue the bottom nylon shock cord directly to

the motor tube to link the mount to the piston. Additionally, I positioned the centering rings

where the fins would fit snugly between the rings in their respective slots. On a recommendation

from Mr. Sharrock, I used marine epoxy to adhere the motor mount inside the body tube and the

fiberglass fins in their slots. I allowed the epoxy to cure before tying the bottom shock cord to

the piston, and from there I looped and knotted the top shock cord onto the parachute and linked

it to the piston.

        At this point, I believed I was almost finished with the rocket until I realized I had not

integrated an altimeter section in my original design. On a typical TARC rocket, the payload

section includes an altimeter compartment, but I completely neglected the fact that my project

proposal contained an altitude requirement for my rocket. The first week of March, Mr. Sharrock

and I started brainstorming about the altimeter section design. We thought we had devised a

decent setup consisting of PVC tubing and an eye hook until I actually purchased the supplies. It

turned out that it would be impossible to access the altimeter because both ends of the PVC pipe

would have to be sealed in ordered to function correctly. Since I did not want to spend any more
Blackwell 5


money, I finally came up with the current design, which essentially extended the nosecone as an

altimeter compartment.

       Amazingly, the same week I redesigned the rocket, SoAR announced it would be

rescheduling its “Georgia Rockets in the Sky” (GRITS) launch for Saturday, March 31st, at

TurfSouth Sod Farm in Lilly, GA (three-and-a-half hours away), instead of April 14 th at a

cornfield in Ranger, GA (an hour-and-a-half away) because the cornfield owner sold his farm in

February. Since the 31st was the beginning of Spring Break, I seized the opportunity and

completed the rocket ahead of time.

       Regardless of the altimeter issue, the most significant obstacle of this entire project

proved to be not the rocket itself but Mother Nature. The Thursday before GRITS, I contacted

SoAR’s president, Mr. Jorge Blanco, who assured me the launch would continue as long as the

forecasted rain chance remained low. My dad and I got up early that Saturday to drive to Lilly,

but we had not reached Macon before the sky clouded over. The weather only worsened the

further south we drove, and we finally arrived around 10 A.M. to torrential downpours and a

dangerously muddy driveway to the launch site. Mr. Blanco informed us that he and the other

people present planned to wait until noon for the rain to cease. Dad and I slept in our truck until

about 11:15 A.M., constantly receiving weather updates from my mother whenever phone

reception was available. Around this time, I remembered Coach Smyrl talking about a club in

Talladega, AL, that hosts launches at the end of every month. I found what I thought was a

phone number and address for the club (Phoenix Missile Works, or PMW), on the NAR website

during one of the reception spurts, and informed Mr. Blanco of our plans. Unexpectedly, he was

very adamant that I should do whatever I could to get my certification flight that day and wished

Dad and I luck!
Blackwell 6


       Using our trusty GPS, Dad and I set out back toward Byromville before we headed

northwest toward Columbus. During a pit stop in Montezuma, I figured out that the GPS

displayed our expected time of arrival at 3:30 P.M. …Central time, meaning we had a four-hour

drive ahead of us. As far as getting to the address on the website, the drive was fairly uneventful,

although we passed through Fort Benning, and I got to see more of east-central Alabama than I

ever thought I would. Following the GPS, we drove to PMW’s registered address, which turned

out to be the treasurer’s home in Ashville, a small town outside Gadsden and the absolute wrong

side of Interstate 20! Dad and I drove into Downtown Ashville about 4:30 P.M. Central time, and

while I called Mr. Sharrock for directions, Dad logically found the fire station and asked the

firefighters for directions. As it turned out, we had driven about 45 minutes out of the way, but

both Mr. Sharrock and the Ashville firefighters were able to access PMW’s website and get us

directions. We arrived at PMW’s cornfield around a quarter after five only to find out that I had

to register with Tripoli Rocketry Association to be able to launch. However, I managed to meet

some of the most helpful people on earth there, and luckily my “emergency” money covered the

membership fee, and I placed my rocket on the pad in under 30 minutes. As if there were butter

on the launch rod, the rocket lifted off and soared into the Alabama sky to the cheers of my swift

acquaintances. The ejection charge performed flawlessly, and the rocket floated gently down to

the field; Dad and I spent about 20 minutes looking for it, though, because the parachute landed

in a puddle. I triumphantly carried the completely unscathed rocket back to the PMW tent for a

final evaluation.

       To my surprise, the PMW folks informed me about the certification reciprocities between

Tripoli and NAR, so in effect I became a member of national and international rocketry

organizations while gaining significant privileges from both. On the other hand, I expanded my
Blackwell 7


amateur rocketry experience into a realm that falls more under engineering research and

simultaneously dealt with likable people along the way. As an added bonus, I essentially

solidified my near-obsessive attention to detail, but most importantly, I got the opportunity to

spend the entire day with Dad and truly show him how interested I am in studying aerospace

engineering as I enter Georgia Tech this coming fall.

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How NASA engineers and high-power rocketry helped one student's research project

  • 1. Blackwell 1 Cody Blackwell Mrs. Corbett AP English Lit/Comp 18 April 2012 High-Power Rocketry “Research is what I am doing when I don’t know what I’m doing.” It may surprise you that I began this presentation with that statement, but I am only repeating a quote from our nation’s most celebrated rocket scientist, Dr. Wernher von Braun. Through the Army Ballistic Missile Agency (ABMA), Dr. von Braun and an extremely bright team of engineers and researchers revolutionized America’s defense and space exploration technology as we know them. ABMA’s research proved most instrumental to NASA’s Apollo program, but, as with any substantial scientific strides, the program had its flaws. More specifically, my research paper discusses the events leading up to Apollo XIII and how Jim Lovell, Fred Haise, and Jack Swigert survived for nearly six days after two oxygen tank explosions in the command module. I plan to study aerospace engineering, and in keeping with the problem-solving spirit, I focused on the ingenious valve NASA engineers developed from duct tape, plastic bags, and cardboard that supplied the three astronauts enough oxygen to return safely home. One might ask, “How can Apollo XIII possibly relate to high-power rocketry?” When I first received instructions for this project, I considered researching techniques for integrating gravity-fed cooling systems into nuclear plants in the wake of the Fukushima Daiichi disaster but ruled it out after assessing its practicality. Building on this practicality, I realized it made much more sense if I built on my prior experiences, namely in amateur rocketry. I have been a member of Creekview Aeronautics Club for the past four years, and our teams have only used relatively
  • 2. Blackwell 2 low-impulse engines in our rockets for Team America Rocketry Challenge. High-power rocketry (HPR), on the other hand, is an entirely different ball game, and I chose to build and launch a high-power rocket specifically because it requires meticulousness and considerably more time than anything the Aeronautics Club does. Accordingly, I encountered an issue I will discuss momentarily which presented an almost project-ending conundrum requiring me, like Mission Control, to work with what little supplies I had. As I learned from members of Southern Area Rocketry (SoAR)—our local National Association of Rocketry (NAR) chapter—and namely Mr. Todd Sharrock and Coach Tim Smyrl, a HPR certification is a prized possession among hobbyists and university clubs. For example, NAR Level I certification (my goal) authorizes flight privileges for rockets weighing over 53 ounces (3.3 pounds), with total impulses between 160.01 Newton-seconds and 640 Newton- seconds, and/or engines not classified as “model rocket motors.” I figured if I could push myself to achieve Eagle Rank, building and flying a high-power rocket for said authorization would be no problem. But like the trail to Eagle, this project required a dedicated mentor, an accountability coach who would scrutinize any changes I made before approving them. As a charter member of the Aeronautics Club and a team captain for the past three years, I know both Mr. Sharrock and Coach Smyrl well. However, I selected Mr. Sharrock because he taught my freshman biology course and our lunch periods happened to coincide this year. Over the past seven months, we met regularly to discuss design options, component suppliers, and any problems I encountered along the way. Consequently, the essence of engineering commands careful consideration and consultation before any project commences. For several days in December, Mr. Sharrock and I discussed his and Coach Smyrl’s successful Level I designs as well as reliable component
  • 3. Blackwell 3 vendors. Finally settling on Public Missiles Limited (PML), I began designing my rocket using Apogee Components’ RockSim 9.0 software, basing the prototype off a PML parts list in the software’s database. I simultaneously researched high-power rocket plans and stumbled across a recovery system I had never seen. Since the Aeronautics Club’s inception, we have attached one parachute each to our rockets’ payload and airframe sections, allowing the two to return separately to the ground. However, the system I found and eventually utilized is a single-chute design using a piston that eliminates the need for a black-powder ejection charge. This system allows for the parachute to be linked with the piston and nosecone by a shock cord and stored without any wadding between the piston and the nosecone; the reloadable motor’s delay forces the piston, parachute, and nosecone out of the tube, keeping all parts of the rocket together during its descent. The only flaw was that I could not use a launch rail system like Mr. Sharrock’s rocket because the guide pins would obstruct the piston. Regardless, I showed Mr. Sharrock and Coach Smyrl, who both heartily recommended it because they have never tried it themselves. Regarding the rest of the rocket, I incorporated the same motor mount design we use in Aeronautics Club with the exception of the motor retainer, which NAR strongly encourages hobbyists to use for high-power rockets, and the number of fins (three instead of four). I settled on slotted phenolic tubing, a hardened parabolic nose cone, and fiberglass fins so, as Mr. Sharrock pointed out, I would at least have something to show in case of a catastrophic failure! Thankfully, all of the parts shipped together over Christmas break. Around that time, I also researched the different types of reloadable motors supplied by AeroTech Consumer Aerospace and Cesaroni Technology, Inc. Again, my membership in the Aeronautics Club exposed me to AeroTech reloadable motors; however, our brand new reloads were not
  • 4. Blackwell 4 performing well at the time, and Cesaroni seemed to offer a much higher-quality lineup of 29 mm-diameter motors for substantially lower prices. Using RockSim-generated flight predictions for comparable motors and data sheets provided by AeroTech and Cesaroni, I determined the Cesaroni H87-12A, with an average thrust of 87 Newtons and a 12 second delay, was most suitable for my certification purposes. Assembling the rocket did not prove too difficult, thanks to my prior experiences, and I started from the bottom up. The motor mount consisted of two customary plywood centering rings, one of which had a slot cut into it so I could glue the bottom nylon shock cord directly to the motor tube to link the mount to the piston. Additionally, I positioned the centering rings where the fins would fit snugly between the rings in their respective slots. On a recommendation from Mr. Sharrock, I used marine epoxy to adhere the motor mount inside the body tube and the fiberglass fins in their slots. I allowed the epoxy to cure before tying the bottom shock cord to the piston, and from there I looped and knotted the top shock cord onto the parachute and linked it to the piston. At this point, I believed I was almost finished with the rocket until I realized I had not integrated an altimeter section in my original design. On a typical TARC rocket, the payload section includes an altimeter compartment, but I completely neglected the fact that my project proposal contained an altitude requirement for my rocket. The first week of March, Mr. Sharrock and I started brainstorming about the altimeter section design. We thought we had devised a decent setup consisting of PVC tubing and an eye hook until I actually purchased the supplies. It turned out that it would be impossible to access the altimeter because both ends of the PVC pipe would have to be sealed in ordered to function correctly. Since I did not want to spend any more
  • 5. Blackwell 5 money, I finally came up with the current design, which essentially extended the nosecone as an altimeter compartment. Amazingly, the same week I redesigned the rocket, SoAR announced it would be rescheduling its “Georgia Rockets in the Sky” (GRITS) launch for Saturday, March 31st, at TurfSouth Sod Farm in Lilly, GA (three-and-a-half hours away), instead of April 14 th at a cornfield in Ranger, GA (an hour-and-a-half away) because the cornfield owner sold his farm in February. Since the 31st was the beginning of Spring Break, I seized the opportunity and completed the rocket ahead of time. Regardless of the altimeter issue, the most significant obstacle of this entire project proved to be not the rocket itself but Mother Nature. The Thursday before GRITS, I contacted SoAR’s president, Mr. Jorge Blanco, who assured me the launch would continue as long as the forecasted rain chance remained low. My dad and I got up early that Saturday to drive to Lilly, but we had not reached Macon before the sky clouded over. The weather only worsened the further south we drove, and we finally arrived around 10 A.M. to torrential downpours and a dangerously muddy driveway to the launch site. Mr. Blanco informed us that he and the other people present planned to wait until noon for the rain to cease. Dad and I slept in our truck until about 11:15 A.M., constantly receiving weather updates from my mother whenever phone reception was available. Around this time, I remembered Coach Smyrl talking about a club in Talladega, AL, that hosts launches at the end of every month. I found what I thought was a phone number and address for the club (Phoenix Missile Works, or PMW), on the NAR website during one of the reception spurts, and informed Mr. Blanco of our plans. Unexpectedly, he was very adamant that I should do whatever I could to get my certification flight that day and wished Dad and I luck!
  • 6. Blackwell 6 Using our trusty GPS, Dad and I set out back toward Byromville before we headed northwest toward Columbus. During a pit stop in Montezuma, I figured out that the GPS displayed our expected time of arrival at 3:30 P.M. …Central time, meaning we had a four-hour drive ahead of us. As far as getting to the address on the website, the drive was fairly uneventful, although we passed through Fort Benning, and I got to see more of east-central Alabama than I ever thought I would. Following the GPS, we drove to PMW’s registered address, which turned out to be the treasurer’s home in Ashville, a small town outside Gadsden and the absolute wrong side of Interstate 20! Dad and I drove into Downtown Ashville about 4:30 P.M. Central time, and while I called Mr. Sharrock for directions, Dad logically found the fire station and asked the firefighters for directions. As it turned out, we had driven about 45 minutes out of the way, but both Mr. Sharrock and the Ashville firefighters were able to access PMW’s website and get us directions. We arrived at PMW’s cornfield around a quarter after five only to find out that I had to register with Tripoli Rocketry Association to be able to launch. However, I managed to meet some of the most helpful people on earth there, and luckily my “emergency” money covered the membership fee, and I placed my rocket on the pad in under 30 minutes. As if there were butter on the launch rod, the rocket lifted off and soared into the Alabama sky to the cheers of my swift acquaintances. The ejection charge performed flawlessly, and the rocket floated gently down to the field; Dad and I spent about 20 minutes looking for it, though, because the parachute landed in a puddle. I triumphantly carried the completely unscathed rocket back to the PMW tent for a final evaluation. To my surprise, the PMW folks informed me about the certification reciprocities between Tripoli and NAR, so in effect I became a member of national and international rocketry organizations while gaining significant privileges from both. On the other hand, I expanded my
  • 7. Blackwell 7 amateur rocketry experience into a realm that falls more under engineering research and simultaneously dealt with likable people along the way. As an added bonus, I essentially solidified my near-obsessive attention to detail, but most importantly, I got the opportunity to spend the entire day with Dad and truly show him how interested I am in studying aerospace engineering as I enter Georgia Tech this coming fall.