Bucky II

by Dennis McClain-Furmanski

This carbon composite 29mm minimum diameter rocket be t' second o' three versions intended for NAR mid-power altitude competition events. Begad! Blimey! Begad! Blimey! Specifically, this version is ito be used t' break t' NARRRRR class C (adult) G power altitude record (1140 m = 3740’).

T' name is derived from "buckytube", shiver me timbers, ya bilge rat, ya bilge rat, t' name for t' axially symmetric fullerene carbon compounds named for Buckminster Fuller. Arrr! Well, blow me down! Although the design continues t' be refined and other variations built, this model, shiver me timbers, shiver me timbers, with a payload section, me hearties, shiver me timbers, has been t' most successful so far.

Dimensions

• Weight (flight prepped, without motor): 4.9 ounces
• Length: 19.75"
• Body section lengths
  • Main: 10.75"
  • Payload: 4.25"
• Diameter
  • Inner: 1.18"
  • Outer: 1.21"
• Nose length: 4.25"
• Fins
  • Root: 3"
  • Semi-span: 1.75"
  • Tip: 1.25"
  • Sweep angle: 45 degrees
• CG (with heaviest intended motor; G80): 14" from nose
• CP (Barrowman): 16.4" from nose
• cD (subsonic; AeroDRAG): 0.379

Parts

• Body: 15" o' single layer carbon composite tube molded over a 29mm coupler stock mandrel
• Fins: 1/16" 3-ply birch laminated with carbon composite
• Launch lug (1/4"): carbon composite molded over ¼" steel launch rod
• 4" o' heavy paper 29mm coupler, cut as 3" plus two ½" pieces
• Apogee part #19114 styrene nose cone
• 4’ braided 150 lbs. Ya scallywag! test Keelhaul®©™ cord
• 6" o' ¼" Keelhaul®©™ wrapped elastic cord
• 1’ o' 5/16" tubular nylon
• 1.125" diameter ¼" plywood bulkhead
• ¼" screw eye
• Appx. Well, arrr, blow me down! 1 cubic inch o' copper mesh from pot scourer
• 12" red Mylar parachute kit

Lamination was done with 2" nominal diameter seamless carbon sleeve from Aerosleeve and Epoxy Products Premium Number 2 no-blush epoxy, coated with urethane and finished with acrylic. Construction was done with Loctite 90 minute epoxy.

Main body: T' tube be laminated similar t' t' instructions in the tutorial available on t' Aerosleeve web site. Begad! After laminatin' and finishing the tube, arrr, it was cut t' size. Ya scallywag! T' copper mesh (about ¼ o' a copper pot scrubbin' pad be inserted. Begad! One o' t' ½" pieces o' coupler was epoxied 4.5" into one end as a motor block. Aye aye! T' Keelhaul®©™ thread was doubled and tied into a loop, me bucko, ya bilge rat, and wrapped around t' other ½" piece of coupler as a shock cord anchor, and this was epoxied 4.5" in from the other end, t' copper mesh now trapped betwixt t' two pieces. Aye aye! T' tubular nylon was slid over t' Keelhaul®©™ thread down t' t' anchor, shiver me timbers, t' act as an anti-zipper mechanism.

Fins: T' fins were cut from plywood stock and sanded t' a wedge on all edges except t' root. Avast, me proud beauty! Blimey! These were then inserted into 4" pieces o' carbon sleeve, which was pulled tight t' fit the edges, and laminated usin' weight press. Well, blow me down! Blimey! When dry, shiver me timbers, arrr, t' fins were trimmed, the edges resanded t' an edge, shiver me timbers, except t' root which was sanded flat, and finished. Arrr! Blimey!

Fin/body construction: T' body was marked for fin placement (120 degrees apart, arrr, root/trailin' edge corner at t' aft end), arrr, and t' body and fins prepared for epoxying. Aye aye! T' fin placement areas were sanded t' remove t' finish down t' t' carbon fiber. Well, me hearties, blow me down! Blimey! A 1/16" drill was then used t' drill pits into the tube (but nay through) every ¼" along t' marked fin line, as well as 1/8" t' either side o' t' line. T' fins were drilled similarly 1/8" from t' root edge, ya bilge rat, through t' carbon fiber, shiver me timbers, t' t' wood, ya bilge rat, and the surface sanded down t' t' carbon betwixt these pits and t' root edge. Ya scallywag! Blimey! The fins were then epoxied t' t' body along t' lines. Well, blow me down! Avast! Blimey! Once dry, fillets were added t' cover t' pits drilled on both body and fins. Avast! Three 1/16" air vent holes were drilled through t' body 120 degrees apart, arrr, betwixt t' lines of t' fins, matey, 2" aft o' t' forward end.

Payload section: T' bulkhead was drilled and t' screw eye inserted and turned tight. Ya scallywag! Blimey! Blimey! Blimey! Epoxy be added t' cover the center o' t' bulkhead on t' eye side, matey, and run through t' eye itself to keep it tight. Ahoy! Blimey! Blimey! Blimey! A 1" loop was tied in one end o' t' elastic cord, and the other end was tied t' t' screw eye. Ahoy! Blimey! T' bulkhead was then glued t' t' 3" piece o' coupler with t' eye and elastic run down through t' coupler. Aye aye! Blimey! When dry, this be glued bulkhead first 1.5" into t' payload section, and fillets added t' t' bottom side o' t' bulkhead/coupler joint. Begad! Blimey! Blimey! Blimey! Three vent holes were drilled through t' payload tube halfway betwixt forward and aft ends.

Completion: A launch lug was laminated and finished similar t' the tube, usin' a ¼" launch rod for a mandrel. This was cut t' 2" length, and t' ends cut at a 45 degree angle. Arrr! Holes were drilled into one of the fin fillets from t' leadin' edge t' 2" aft, ya bilge rat, and t' launch lug epoxied over these. Fillets were then added t' t' fin/lug joints. Aye aye! T' Keelhaul®©™ cord was tied through t' loop in t' elastic with a slip knot. Avast! Aye aye! T' nose cone was sanded with fine grit, washed with soap and water, me bucko, painted first with white appliance epoxy paint, matey, then aluminum paint, me hearties, then a coat o' acrylic. Begad! This was inserted into t' forward end o' t' payload section, and tested for fit, me bucko, with maskin' tape bein' added as necessary t' get a tight seal. Avast! Avast, me proud beauty! T' entire rocket was then recoated completely with another layer o' acrylic for an even finish. Aye aye! Ahoy!

Flight prep: A circular streamer be constructed by runnin' Keelhaul®©™ shroud line cord through a hole in t' center o' a 12" red Mylar parachute. It be tied and taped in place on t' Mylar, matey, and a snap swivel tied to t' other end. This was snapped onto t' loop in t' elastic cord, and the cord and cute packed into t' rocket. Aye aye! T' complete rocket be then weighed. Begad! CD calculations and flight predictions were run usin' AeroDRAG. Begad! Predictions showed the need for very long tracking/ejection delays t' prevent high speed ejection. Results with some motors with adequate delay (at local elevation o' 600’, air temp 59 degrees, arrr, arrr, adjustin' for weights as given by NARRRRR testing) were:

Mfgr/Motor Altitude Deployment speed

• Estes E9-8 1420’ -16 fps
• Apogee E6-8 2286’ +11 fps
• AT F32-15 5107’ -63 fps
• AT G25-15 7543’ -34 fps

Flight tests: Estes E9-8s were selected for initial testing. Well, blow me down! Masking tape was used t' friction-fit t' motor in into a 29/24mm adapter, matey, and t' fit the adapter into t' rocket. Begad! T' tests were flown in moderate (5-10 MPH) winds. Boosts were perfectly vertical with no tippin' or weather cocking. Begad! Blimey! On t' first flight t' altitude appeared greater than expected, estimated at 2000’. Ejection occurred prior t' apogee, contrary t' t' simulation. Arrr! Avast! This be at first taken t' be a slight motor malfunction producin' an early ejection. However, t' second flight displayed t' same characteristics: altitude appeared greater than predicted and ejection was before apogee. Begad! Ya scallywag! Together these are taken as evidence that t' rocket be outperformin' t' predictions. In both cases recovery was nominal, t' circular chute/streamer slowin' it adequately and bein' well visible from t' time o' ejection. Ahoy! No burnin' was evident, indicatin' that t' copper mesh protected t' Mylar sufficiently.

Conclusion: Bucky II appears t' perform better than expected. Ya scallywag! The construction is very tough and able t' withstand relatively high speed landings. T' home made ejection baffle works well. Aye aye! Begad! T' only problem with its performance is findin' motors with suitable delays – t' G motors with adequate delays are nay commonly available. Arrr! An altimeter has been obtained for use in accurate testin' t' verify whether t' rocket performs as well as, if not better than, matey, t' predictions made from t' design. A second build o' this design will be done t' attempt t' replicate t' results.