| Guest Editorial: The FAA rolls the dice... |
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and there are winners to console the losers.
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| Editorial by PAT GORDZELIK | |
| Thursday, April 02, 2009 | |
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Note: The references and data in this article were furnished by several people, including Art Upton, Darrell Mobley, David Reese, and several others I am grateful to. Brent McNeeley, editor/publisher of Extreme Rocketry, as well as Neil McGilvray and Bob Utley, editor/publisher of ROCKETS Magazine, have both agreed to publish this article in each of their respective publications, transcending personal interest and embracing hobby concerns first. The article can also be found after the magazines are distributed on www.rocketryplanet.com and www.rocketryonline.com.
For most people, the recent FAA Final Ruling has reduced regulation, by eliminating bothersome notification for rockets below 3.3 pounds (Class 1). Class 2 activities will require a waiver, but that should not present much difficulty. This result can be safely attributed to the 50 year safety record of organized hobby rocketry and the organizations like NAR and TRA, working in concert with our partners, the FAA. But for some people, it still hasn't sunk in that the new FAA Final Ruling has severely handicapped the individuals who routinely fly research motors or multiple commercial motors in the impulse ranges above O impulse. The new Class 3 rockets that have installed greater than O impulse must meet a plethora of criteria just to have the flight plan approved, regardless of whether it is a low altitude Pyramid or a minimum diameter high performance bird. At first blush, many high power rocketeers will say, "Who cares? I don't fly above an O motor." Sure, but do you cluster? 4 M's? A pair of N's? If the total impulse of the flight is greater than 40,960NS, then you will be bumped up to Class 3 where you no longer benefit from the umbrella waiver of the launch organizer and may be required to file your OWN waiver application at least 45 days in advance, or at least get your data to the waiver holder with the following requirements: When a Class 3 - Advanced High-Power Rocket requires a certificate of waiver or authorization the person planning the operation must provide the information below for each type of rocket to the FAA at least 45 days before the proposed operation. The FAA may request additional information if necessary to ensure the proposed operations can be safely conducted. The information shall include for each type of Class 3 rocket expected to be flown:
* Paragraph (a) requirements:
This fundamental change makes the typical Level 3 documentation requirements look pale by comparison, as possibly EVERY launch of a Class 3 rocket may require even more documentation than an L3 flight would require. This shifts the responsibility off of the launch organizers and puts it squarely on the backs of the flier and waiver holder. One of the more confounding requirements is filing all data 45 days in advance of each type of rocket, which would include data readings of winds aloft. Care to guess what the winds aloft will be 45 days in the future? One can suppose the NOAA historical winds aloft data or recent GOES wind data would be accurate enough to input to the model and return results which qualify for the FAA requirements. But the inputting of that data seems redundant 45 days prior. On site, perhaps the high altitude winds-aloft data for popular large launch sites (Black Rock, Delamar, Wayside, Argonia, etc.) could be tabulated in an easier-to-use format? For lower altitude Class 3 flights at other, smaller sites, the aviation weather service is able to give real-time and forecast winds-aloft data for nearby airports; tracking the trends over time and using those results may be suitable as well. "This begs the question. Is there any commercially available 6DOF splash pattern software which meets the FAA requirement?" This begs the question. Is there any commercially available 6DOF splash pattern software which meets the FAA requirement? That seems to be the biggest hurdle in the rules. Aside from RS-Pro, I was not able to find one that I believe will satisfy the FAA. At $1000.00 a copy, that may be a little steep for most fliers. The real question is why the impulse change was made. The FAA discussion claims:
I searched the docket and found only one person who recommended the change to 40,960 N-s. In the TRA Research code, individuals can fly up to full P impulse (81920) without Board review. My suggestion when applying for waivers is to request the cap for Class 2 be increased to 81920 N-s, especially if your site has a safe history of previous flights at that impulse at your granted altitude. Also, it is possible that the concern about the extra documentation for Class 3 flights is exaggerated. The new regulations do not require extra documentation for each flight or each rocket, but rather for each type of rocket (same exact wording as is used for Class 2 rockets), so a club may seek a blanket waiver for Class 3 flights that answers those questions once. In my previously mentioned conversations with Mr. Brinkman, that was not hammered out. But, according to the published rules.
The other concern is the requirement of launch site size as per altitude requested. While it is prudent to want to protect uninvolved people, one quarter to altitude, say, for Wayside's past granted altitudes of 50000', equates to no highways or non launch site owner homes be closer than 2.37 miles.
As I said, there are many winners in these new regulations, but there will be a few hills to climb for some as well. Finally, see below a sample form for Class Two Waiver applications. I hope it helps you in applying for your new 2009 waivers. If you have already been granted your 2009 waiver prior to the effective date of this ruling of February 2, 2009, the new regulations will not affect you, according to Mr. Brinkman.
Finally, I believe that this ruling will be a learning process for both the HPR enthusiast and the FAA. I also believe that the FAA is one of the best Federal Agencies I have ever dealt with, one that reasonably makes efforts to serve any questions we may have, and have historically been very accommodating. Happy Flying Pat Gordzelik Pat Gordzelik is long-term hobby rocketry enthusiast known for his passion for propellant and lives in the Texas Panhandle with his wife Retta. Pat also serves as a board member on the Tripoli Rocketry Assocation Board of Directors. |
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I think you meant "rolls," right?
To me the use of the word "impact" rather than "landing" (plus the mention of spent motors and discarded hardware) implies ballistic impacts with no recovery system. That being the case then none of the rockets will have a nominal impact area because they are required by safety code to have a recovery system. Therefore no fancy 6DOF simulations would be required.
The use of the word "nominal" would also preclude speculation about failure modes as those are of course not normal.
-Aaron
To me the use of the word "impact" rather than "landing" (plus the mention of spent motors and discarded hardware) implies ballistic impacts with no recovery system. That being the case then none of the rockets will have a nominal impact area because they are required by safety code to have a recovery system. Therefore no fancy 6DOF simulations would be required.
The use of the word "nominal" would also preclude speculation about failure modes as those are of course not normal.
Although the definitions from that chapter do not apply to Part 101, the FAA based their Class 3 requirements on existing practice so this should provide insight into what they want. Of course a pointed question or two for the FAA would clarify things. It may be that they include normal landings under parachute as "impacts". It would be nice if that were the case if they clarified how this data was to be generated and what assumptions should be used. Note that the definition of "instantaneous impact point" in Chapter III excludes atmospheric drag effects.