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REV 2.4 - Thu Jan 13 02:35:59 2011

Scratch
Competition Payloader
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SPECS: 14.8" x .7362" - 0.9 oz
ROCKSIM FILE: Right Click to Download
SpaceCAD FILE: MISSING - please submit here
REC'D MOTORS: MISSING - please submit here

(Contributed - by Chan Stevens [Who's Who Page] - 12/04/05) (Scratch) Competition Payloader

Brief:
For an R&D project I was doing for NARAM-47, I needed to fly at least 12 flights and record altitude for each flight using a Perfectflite Alt15kWD altimeter. The rocket needed to be rugged, handle the altimeter payload, and support being quickly prepped and flown so that I could get all the flights in as quickly as possible. It also needed to be as high performance as possible, since the experiment was to analyze competition-style rockets.

Construction:
From my spare parts stash:

  • Polystyrene nose cone from ASP, size BT-20
  • BT-20, two 6-inch sections
  • 1/16" G10 fiberglass fins
  • 2x20" mylar streamer (party store surplus)
  • Kevlar® shock cord
  • Nomex® heat shield

I used several official EMRR tips on this build including:

  • If a fin breaks off at the fin/ body tube joint, simply carefully sand off the old glue from both the tube and the fin, then reattach.
  • Party streamers. 60 ft for $2.50. Enough for nearly 30 streamers. beats paying $5.00 to Estes to make four?
  • Shock Cord: Use a Kevlar® shock cord root. Also make the bungee at least 2.5 times the length of the BT.
  • Always bring a bottle of medium CA to launches.

The construction is fairly straightforward since it is a basic 3FNC style rocket, so I'll elaborate on the payload construction.

The payload bay is fairly long (6") to accommodate the altimeter and nose cone shoulder plus my homemade bulkhead. Since I was working from spare parts, I made the bulkhead from a tube coupler with a disk cut from basswood. To anchor the shock cord, I tied a knot on one end of the Kevlar® line, slipped it into the payload tube, and then inserted and glued it in the bulkhead. The Kevlar® was then secured between the bulkhead and the body tube. I finished the payload bay by drilling a couple small vent holes, critical for accurate altimeter readings.

The streamer is nested in the lower portion, protected by a Nomex® heat shield. Not only does this take up less room than wadding, but it can be reloaded and prepped for flight in under two minutes (including resetting the altimeter).

Notice that the RockSim file does not include a launch lug. That's because the purpose of the R&D report was to measure the impact of launch lugs on the drag coefficient. The rocket was flown about 12 times without a lug, then a lug was attached to the fin/tube joint and flown again about 12 times on the same types of motors to compare altitudes. To eliminate weather variability, I tried for all flights in the same day. That's 24 flights on one rocket on a single day, many of which were approaching 1700 feet in altitude. Try that feat with a basic E2X kit...

Finishing:
Normally competition-style rockets are not painted, but since I had already lost a previous model (including an expensive altimeter) to 1500-2000ft altitudes on an overcast day, I elected to paint this one florescent orange. That made it much easier to pick up in the sky and on the field. I also sanded it smooth with 600 grit paper and coated with automotive wax to reduce the surface drag.

Flight:
With the fairly small fins, this rocket is only marginally stable with a C6-7, so the altimeter actually provided enough CG shift for very stable flights.

All flights were straight as an arrow, and on a C6-7, my actual readings clustered fairly closely around 1500 feet.

Recovery:
Throughout the day, I suffered a few minor nicks/dings, including breaking a fin loose, and a Kevlar® line break. Remarkably, when the Kevlar® broke, I was able to recover both sections in fairly high grass.

Summary:
PROs: Simplicity of construction, low cost materials, very good performance for a payload carrier, and very durable.

CONs: Not suitable for official NAR payload events (payload must contain a BT-20 tube, so it needs to be slightly larger diameter).

[Submit your Opinion]

GUEST's OPINION:
12/05 - "So, what were the conclusions of your research?" (J.L.)

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[Enter Flight Log]
Date Name Motor Ejection/
Altitude
Wind Notes
07-09-2005 Chan Stevens Est SU A8-3 Just Before 0-5 mph winds Event: NARAM47 R & D flights
18mm - test flight/using a new tower
07-09-2005 Chan Stevens Est SU C6-5 Just Before
(1138 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower
07-09-2005 Chan Stevens Est SU C6-5 Just Before
(1035 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower
07-09-2005 Chan Stevens Est SU C6-5 Just Before
(1058 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower
07-09-2005 Chan Stevens Est SU B6-4 Just Before 0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower/altimeter failed
07-09-2005 Chan Stevens Est SU B6-4 Just Before 0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower/no altimeter reading
07-09-2005 Chan Stevens Est SU B6-4 Just Before 0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower/no reading
07-09-2005 Chan Stevens Est SU B6-4 Just Before
(375 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower/left unstable, near horizontal path
07-09-2005 Chan Stevens Est SU B4-4 Just Before
(508 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower
07-09-2005 Chan Stevens Est SU B4-4 Just Before 0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower/no reading
07-09-2005 Chan Stevens Est SU B4-4 Apogee - NC Up
(483 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower
07-09-2005 Chan Stevens Est SU B4-4 Just Before
(468 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Tower
07-09-2005 Chan Stevens Est SU C6-5 Just Before
(1083 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Rod/pop lug
07-09-2005 Chan Stevens Est SU C6-5 Just Before
(1064 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Rod/pop lug
07-09-2005 Chan Stevens Est SU C6-5 Just Before
(1012 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Rod/pop lug
07-09-2005 Chan Stevens Est SU C6-5 Apogee - NC Up
(1051 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Rod/mounted lug
07-09-2005 Chan Stevens Est SU C6-5 Apogee - NC Up
(965 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Rod/mounted lug
07-09-2005 Chan Stevens Est SU C6-5 Apogee - Perfect
(1036 ft)
0-5 mph winds Event: NARAM47 R & D flights
18mm - Rod/mounted lug
07-28-2005 Chan Stevens Est SU C6-7 Apogee - NC Up
(1588 ft)
5-10 mph winds Model 2 - no lug/tower
07-28-2005 Chan Stevens Est SU B6-4 Very Early
(701 ft)
5-10 mph winds Model 2 -
07-28-2005 Chan Stevens Est SU C6-7 Apogee - NC Up
(1597 ft)
5-10 mph winds Model 2 -
07-28-2005 Chan Stevens Est SU C6-7 Just Before
(1422 ft)
5-10 mph winds Model 2 - Broken fin
07-28-2005 Chan Stevens Est SU C6-7 Apogee - NC Down
(1509 ft)
5-10 mph winds Model 2 -
07-28-2005 Chan Stevens Est SU C6-7 Just Past (1-2sec)
(1451 ft)
5-10 mph winds Model 2 - Broken fin (road)
07-28-2005 Chan Stevens Est SU C6-7 Apogee - Perfect
(1503 ft)
5-10 mph winds Model 2 - Lug
07-28-2005 Chan Stevens Est SU C6-7 Apogee - NC Up
(1626 ft)
5-10 mph winds Model 2 -
07-28-2005 Chan Stevens Est SU C6-7 Apogee - Perfect
(1523 ft)
5-10 mph winds Model 2 -
07-28-2005 Chan Stevens Est SU C6-7 Very Late
(1176 ft)
5-10 mph winds Model 2 - non-vertical flight path, motor/nozzle failure?
07-28-2005 Chan Stevens Est SU C6-7 Just Past (1-2sec)
(1494 ft)
5-10 mph winds Model 2 -
07-28-2005 Chan Stevens Est SU C6-7 Apogee - NC Down
(1470 ft)
5-10 mph winds Model 2 -

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