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Ignitor Team: Go!

  • October 29, 2019June 5, 2020
  • by Dakota

[This is an update from the Ignitor Senior Design team.]

Welcome back! This week, we will walk you through our preliminary plans.

Chosen Method:

After weighing out the risks and benefits of all potential methods, our team chose an industry standard ignition method known as the augmented spark plug system. In short, a portion of the fuel will be diverted from the combustion chamber and injected into a smaller sub-chamber for ignition via spark plug. This resulting fireball will then travel down a channel into the primary combustion chamber and create the thrust necessary to get our rocket off the ground and up to the Karman Line.

Below is an extremely simplified initial diagram:

A block diagram showing the team’s proposal for an augmented spark plug system.

As you can see, this system will require quite a bit of design overhaul on original build. However, we hope that the hours of sweat and tears we put into this system will result in a reusable, economical, and safer rocket.

Project Updates:

Currently, we are working on the first iteration of this new injector. Recently, we started modeling the new sub-chamber which will house the augmented spark igniter system. We are simultaneously working on the chamber geometry, injection elements, and creation of the spark plug itself.

Each of these tasks offer their own set of chanllenges, but we can’t wait to solve them. Past them, we will move on to finalizing the first iteration using SolidWorks. We will then move onto inert water flow tests before actual combustion.

We can tell this project will be a lot of work which will push us to our technical limits. Particularly, crunching all the numbers associated chamber geometry and flow characteristics will take some time. But we plan to give this project everything we have to develop an innovative injector/ignitor system — and get this rocket to space.

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(Remix to) Ignition

  • October 24, 2019June 5, 2020
  • by Dakota

[This is an update from the Ignitor Senior Design team.]

Our Team

Hello everyone! We’re a team of four dedicated and driven individuals trying to make this rocket as reusable and as efficient as possible by improving the injection and ignition system.

  • Lucas Franz (CHE)
  • Kenneth Otten (ME)
  • Rachel Gart (ME)
  • Nicholas Lavigne (CHE)

Lucas is both the Team Lead and Propulsion Specialist. Kenneth’s focus is CAD Specialist and the Design Lead. Rachel is the Manufacturing Specialist, Outreach Coordinator, and Team Manager. Nicholas specializes as Propulsion and Materials Specialist.

You might be asking yourself, “Why did you choose this crazy hard project over some much easier ones?” For us, the answer is easy: We all have passion for space and rocketry, and we all wanted to do something more with our senior design project.

We believe this project provides one of the best ways for us to make an impact, and we’re excited to tell you how we plan to do just that.

Our Goal

Our goal is simple: To incorporate an ignitor into the rocket’s injector. The idea may be simple, but there is some complexity in integrating the ignitor into the rocket.

We also want the ignitor to be reusable. Long-time readers of the blog will know how the first ignitor worked. Every time the ignitor was used, it was consumed. This means a costly reprint every time we ignite the rocket. The ignitor integration team plans to change this and reduce impediments to getting our rocket into the air.

Our Considerations

Briefly, here are a few designs which didn’t make it past the first design stage. Still, they are interesting solutions to the problem at hand.

Laser ignition, while very cool sounding, was impractical for what we were looking for. Lasers are delicate and difficult to work with. Minimum ignition energy also works differently with lasers, since ignition comes not from a spark but instead from exciting the fuel until it ignites.

Image result for laser ignition
A depiction of laser-assisted ignition. (Source: Nature)

We’re working with pretty extreme conditions and would need to have a powerful laser to actually achieve ignition. The time and research costs would be too high, so we need to do something simpler.

We turned to pure chemistry. The image below shows triethylaluminum, an extremely unstable compound which will spontaneously burn when exposed to oxygen. It’s very difficult to work with, but it would certainly simplify design.

Triethylaluminum, a volatile, hypergolic chemical. (Source: Wikipedia.)

Maybe not so “simple,” though. The bonds between the ethyl groups readily and explosively break down in contact with oxygen. We ruled this out due to the red tape and safety concerns of working with such a volatile compound.

Our next blog will outline our current plan.

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…This is Ground Control

  • October 22, 2019June 5, 2020
  • by Dakota

[This is an update from the Ground Control Senior Design Team.]

Greetings from Castle Point Rocketry’s Ground Control team! The team consists of five team members: Martin Gilmartin (MechEng), John Hamill (MechEng), Ed Minnix (CySec), Nicholas Yarbrough (CompEng), and Charles Zwicker (CompEng).

We’re currently working on Revision 2.0 of the Ground Infrastructure Support and Control Systems in order to increase its capabilities, make it more reliable and redundant, and make its operations more logical and streamlined.

Here are some of the improvements we’re making.

Ground Control Station (GCS)

This is the main station that we will use to control the launch sequence, view our camera feeds and telemetry from the rocket (velocity, altitude, etc.), and manually actuate any valves in the event of emergency.

This subsystem will be an upgrade over last year’s setup. We are integrating the control and monitoring into a single unit as opposed to last year’s iteration which was handled by a separate laptop. The combination of these systems with a more powerful computer will lead to easier setup and transport. Furthermore, the new computer will run an enterprise-grade Linux distribution, providing further stability.

The GCS will be upgraded to redundantly store all of the data being streamed in realtime from the Ground Support Station and run for over eight hours on battery power, with a backup generator we can switch to without interruption. We will also waterproof the entire case and its connections so rain won’t hinder our progress.

We’re also constructing an antenna rotator in order to accurately track the rocket as it is airborne and achieve a more reliable signal.

Ground Support Station (GSS)

The GSS will roll all of the pre-launch hardware, which needs to be near the rocket, into one enclosure, streamlining it from its previous iteration. In addition, a large number of the GSS’s computational systems will be integrated directly into the GCS, reducing the hardware required at this location. We will upgrade the cameras and tripods in order to receive a higher quality video. This subsystem will also be battery powered for over eight hours.

Conclusion

We’re currently working with Nathan and Ben in the design and planning phase, ironing out the details before we pull the trigger and begin our first round of purchases. Our next steps include designing initial prototypes in CAD which we will then build and test followed by detailing the components of each system down to the minutia.

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“When is Launch?”

  • October 17, 2019June 5, 2020
  • by Dakota

We get that question a lot. So, rather than keep everybody waiting, here is a quick update.

The short answer is, “Coming soon.” The long answer is much more complicated and balances quite a few variables.

The biggest factor in play is our lack of components. When the team finished testing this summer, it was due to a hairline fissure in our liquid oxygen (LOX) tank. Though barely noticeable to the naked eye, this defect could have caused a catastrophic explosion with further testing. We returned the tank to its manufacturer for analysis and remanufacture, which can be a lengthy process. Additionally, the fins and nose cone arrived after testing. Though not necessary for testing, they need to be added to the rocket before we can launch.

Castle Point Rocketry is also in the middle of a transition. Since the founders are no longer Stevens undergraduates, we are navigating the challenges associated with acquiring real estate and transferring funds. (All while pursuing graduate school or full-time jobs!) Luckily, we have three great senior design teams to help tackle further engineering projects.

The final challenge to a set launch date is the same as last year: permits. Until the rocket passes our eight-step testing process, we cannot apply to launch. Even after applying, we will need to wait for approval — and maybe return for more tests.

The primary objective is still to put a liquid-fueled rocket beyond the Karman Line. We have some more help getting there, but testing is still in a temporary holding pattern.

So all that is to say: “Soon. Very soon.”

Uncategorized

New Senior Design Teams

  • October 17, 2019June 5, 2020
  • by Dakota

Last month, we mentioned the most exciting news from Castle Point Rocketry. In short, the company is sponsoring three new senior design teams to work on the rocket.

These interdisciplinary teams incorporate students from all across Stevens Institute of Technology. Chemical (CHE), Computer (CPE), Electrical (EE), and Mechanical (ME) Engineers will work with Cyber Security (CS) students to help us reach the Karman Line.

As with last year’s marathon goal, a diverse set of subsystems is on the docket. Here is a quick look.

Flight Computer Team

Redundant hardware is beneficial for most projects. If one component on a flight computer fails, the entire system may shut down. (Or, in the case of a rocket, end catastrophically.) This team will incorporate fallback systems into the current computer in order to make a more robust rocket.

The Flight Computer Team will design a leaner flight computer for Castle Point Rocketry. Composed of two EEs and a CPE, they are well-equipped for the task.

Ground Systems Team

The Ground Systems Team will remodel the ground infrastructure required to launch the rocket. Suitably, two CPEs, two MEs, and one CS are tackling this sprawling project.

Most radically, upgrades will be made to on-site telemetry systems and relay boxes. These changes will allow the team to communicate with the rocket more reliably and more securely. This is necessary both pre- and post-launch.

Given the time, the team will also build a stronger ground control center to provide instant feedback on the rocket.

Igniter Team

Expanding on last year’s prototype, the Igniter Team is designing a new igniter. After all, our current igniter is not reusable — though it looks spectacular in action. The goal of this project is to make it reusable and safer.

Two CHEs and two MEs will make it happen. Already, a series of meetings has been very productive. If all goes well, it could even be on the next injector model!

Future Blogs

In the future, both the company and these new teams will provide blog updates. That way, we can keep everyone informed of the latest news at Castle Point Rocketry!

News

Paying It Forward

  • September 11, 2019June 5, 2020
  • by Dakota

Over the last year, Castle Point Rocketry has learned a lot. We built a rocket, created a company, and maintained a brand — all while keeping afloat in school. Now, it’s time to look to the future.

The eight founders of Castle Point Rocketry have graduated from Stevens Institute of Technology, but the relationship is far from over. This year, Castle Point Rocketry is sponsoring three more year-long senior design groups at Stevens. They will each work on a small section of the rocket, iterating on the current design to make a better vehicle overall. The goal is still the same: To create and launch a liquid-fueled rocket to the Karman Line.

We look forward to what this partnership holds in store. The mere fact that the project has generated interest in Stevens graduates-to-be is promising in and of itself!

Uncategorized

The Faces of Castle Point Rocketry

  • July 12, 2019June 5, 2020
  • by Dakota

It’s high time we re-introduce everyone who makes up this team. After all, once we test this thing and get our big media break, you’ll want to know who we all are.

Team Members

A core group of eight have been with this project since the beginning. We have four Mechanical Engineers (ME), two Chemical Engineers (CHE), one Computer Engineer (CPE), and one Computer Scientist (CS). Pictures and short blurbs below.

  • Abraham Edens (ME)
  • Thomas Flaherty (ME)
  • Faris Ibrahim (CPE)

Abe is our Aerodynamic Design and Mathematics Specialist. He helped solve the regenerative heating problem and worked with Tom and Will on many manufacturing tasks.

Tom also specializes in computer-aided design (CAD). He spent innunerable hours modeling an injector to Monica’s and Dakota’s specifications before tackling other projects.

Faris, working on Electronics, Signals, and Avionics, was integral to designing the team’s circuit boards and developing how those systems fit into the rocket.

Unfortunately, Abe, Tom, and Faris are unable to join the other members of the team for testing. However, we are still very proud to call them members of the Castle Point Rocketry team — we couldn’t have done it without them!

  • Benjamin Iofel (CS)
  • William Skwirut (ME)
  • Nathan Tahbaz (ME)

Ben is Lead Programmer, meaning he has literally written the code for our testing procedure. Recently, Ben has also branched out to become our resident electronic hardware expert.

Will is formally the Machining Specialist, but he has extensive knowledge of (and a quippy remark for) for nearly every facet of the project. He also played a large role in designing the plumbing system.

Nathan is the true Renaissance Man of the group. As Team Lead, it’s his job to ensure every subsystem is stitched together — on top of serving as Point of Contact for purchasing and inquiries.

  • Monica Traupmann (CHE)
  • Dakota Van Deursen (CHE)

Monica and Dakota, Propulsion Specialists, collaborate to fill our propulsion and PR needs.

Monica, who is also our Safety Officer, designed our plumbing system with Will and Dakota, manages our social media presence, and interfaces with many of our top donors. Dakota mainly focused on the engine, but he also manages the project’s blogs and attends to the tasks that fall in the ever-present gray areas.

Ben, Will, Nathan, Monica, and Dakota are all on site for this week’s testing procedures.

Team Volunteers

As you may have noticed around campus and online, Castle Point Rocketry has put out a call for volunteers. Two excited Stevens students have come to our aid, and we are very grateful!

  • Daniel Cooke, Avionics and Telemetry
  • Rodrigo Nogueira, Fabrication

Rodrigo is a graduate student in ME who joined us in early February. His extensive background in fabrication and manufacturing have come in handy many a late night.

Dan, a rising junior in CPE, joined us at the beginning of the summer. He has been a great help to Ben in preparing our electronic systems for integration and testing.

Rodrigo is on site for this week’s testing procedure, and Dan may be coming down over the weekend.

Industry Advisors

We are also lucky to have had the input of two professional aerospace engineers. Rich Kelly from Valcor Engineering and Luke Colby from Triton Space Technologies have thankfully withstood a barrage of phone calls and emails from the team.

Luke (back row, middle) and Rich (back row, second from right) visiting the team in Hoboken.

Rich and Luke are both on site for this week’s testing procedures.

Uncategorized

Dolly Upgrade!

  • June 25, 2019June 5, 2020
  • by Nate

Initially, we built a dolly out of 80/20 aluminum to wheel about the rocket. This dolly proved to be too short as our rocket got longer. So, we decided on an upgrade — wood! This new dolly is double the length of the previous.

Abe fills the new dolly’s tires with more air so it works extra-well.

Over time, our rocket has only gotten longer. (At least, after it’s initial shortening when we moved from a two-stage system to a one-stage system.) Our rocket is around 25 feet long. This dolly will be used to transport it around the test and launch sites.

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Dry Run Test #2 (Teaser)

  • June 14, 2019June 5, 2020
  • by Dakota

It’s June 14th! You’ve caught us mid-test! So, let’s break these last few days down…

4,000 square feet of grass. 2,000 feet of fiber optic cable. 1,200 feet of Caution tape. 770 cubic feet of U-Haul space. 120-volt generator. 30 feet of truss.

10 seconds from the heart of campus. 9 o’clock start time. 8 team advisors. 7 valves. 6 visitors and counting. 5 walkie-talkies. 4 days. 3 structures. 2 tests. 1 fake rocket.

Keep an eye on our Instagram (@cprocketry), Facebook, and blog to see how it goes!

Uncategorized

“Clean For Oxygen Use”

  • June 11, 2019June 5, 2020
  • by Dakota

We can all probably agree with the relative levels of cleanliness. Around the bottom of the scale, there’s “I Am Comfortable Living In This.” A little more clean, you probably find “Company is Coming,” closely followed by “My Parents Are In Town.” Near the top of your list, you probably find “Apartment On The Market.”

“Clean for Oxygen Use” may top the charts. It’s certainly not a household standard.

Bottom shelf: Unclean. Top shelf: Clean.

This cleaning method is the entire reason we constructed our clean room. Much of our rocket will come into contact with high-purity oxygen, whether in liquid or gas form. Gaseous oxygen loves lighting things on fire, and liquid oxygen freezes most substances solid — so we need to be sure everything is as clean as humanly possible. To do so, we have a six-step cleaning process.

Step One: Alcohol Bath

After we identify a subassembly to clean, we remove each piece from storage. We bathe each individual fitting, pipe, adapter, and valve in isopropyl alcohol. (That’s the same alcohol you put on wounds to clean them.) For 12 minutes, they rattle around inside an ultrasonic chamber. By vibrating them very, very quickly, the machine dislodges defects, dust, and other gunk that is clinging to them.

Our ultrasonic bath is located on the left.

Isopropanol is also a dehydrant. This agitation bath ensures every out-of-the-way nook and cranny is water-free. Any water left in the system would freeze in contact with cryogenic liquids, decreasing functionality and making the rocket explosion-prone.

Step Two: Nitrogen Purge

After they’re removed from the bath, each part is individually inspected for remaining debris.

A tee junction during the nitrogen drying cycle.

Then, every part is dried with a pressurized jet of filtered nitrogen. Not only does this ensure no isopropyl alcohol is left on the part, it blows away any remaining foreign materials.

Step Three: Alcohol Rinse

As if Step One weren’t enough, we then subject each component to yet another round of alcohol. This time, the isopropanol is targeted in a stream. The entire part is washed beneath a squeeze bottle before moving on to Step Four.

A tee junction having an isopropyl alcohol shower.

Step Four: Nitrogen Purge

More drying! Like most alcohols, isopropanol is flammable so we need to make sure each part is bone-dry before assembly. This last round of nitrogen is usually enough to get the last bits of stubborn junk off of our fittings.

Step Five: Critical Inspection

Once the second nitrogen blow-down is complete, we are fairly certain nothing remains. But just to be sure, though, we inspect each piece from every angle for leftovers. Inside and outside, nothing is allowed to escape our prying eyes. And on the off-chance we still find refuse holding on? We restart the whole process from scratch. We bought smaller ultrasonic bath just for that purpose.

Step Six: Assembly

Finally, we are sure that our parts are Clean for Oxygen Use. We bubbled, tossed, dried, washed, and dried most everything (and even brushed some with a high-grade pipe cleaner), and it’s time to put the pieces together. One by one, being sure not to stir the air or drop anything, the rocket starts taking shape. We have 24 subassemblies ranging in size from one component to thirteen.

One of the subassemblies we will be using for tank testing.

Each über-clean subassembly is then given a new home on the high shelf in our clean room. Small subassemblies are bagged and given a unique name so they don’t get confused down the road.

And that’s how you make a rocket Clean for Oxygen Use!

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  • New Starts
  • Ignitor Team: Go!
  • (Remix to) Ignition
  • …This is Ground Control
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