Please note: This page gives a
general coverage of the Jetex 50 series motors manufactured by Wilmot Mansour, Sebel and
Powermax. Two further pages give more detailed information about specific motors:
(approx, actual size)
General
Description
By far the most popular of all
the motors, more Jetex 50s have been sold and flown than all the other models
combined. This design, introduced in May 1949, has evolved through several versions,
all of which are detailed on this page.
What is common to all "50" size
engines is the thrust chamber internal diameter of ~0.560 inch (14.22 mm), to fit
standard "50" size (0.5-in [12.7 mm] dia) propellant pellets. All the 50 size Jetex
engines produce substantially the same thrust, averaging on the order of 1/2 to 5/8 ounce
[14.2-17.7 gm], peaking to 7/8 ounce [24.8 gm], or even higher, at the end of the
run. (In other respects, the Jetex 35 is very similar to the Jetex 50 Export and 50B
models.)
Here is a differentiation
summary; each motor is described in greater detail farther below on this page:
Engine
Designation
|
Series
Sequence
|
Year
Introduced
|
Manufacturer
|
Case
Material
|
How
Made
|
Remarks
|
50 (Standard)
|
First Jetex 50 size introduced
|
May 1949
|
Wilmot Mansour
|
Aluminum
|
Machine turned, with shallow ribs
|
Dropped from production in early 1954; flat
nozzle end; ID=14 mm; one spring; no flame shield or exhaust deflector; nozzle diameter
= 0.030" [?]
|
50 Export
|
Improved second version, to better fit
augmenter tubes
|
|
Wilmot Mansour
|
Aluminum
|
Pressed, smooth
|
Rounded, nozzle-shaped end cap to use with
augmenter tubes; no flame shield or exhaust deflector; 29.3mm long; 14mm ID; one
spring; only 2 spring holes in cap
|
50B
|
Third version of the 50 size, with larger
volume for fuse
|
Sep 1953 (Aeromodeller, p 517)
|
Wilmot Mansour
|
Mild steel
|
Pressed
|
Rounded, nozzle-shaped end cap to use with
augmenter tubes; slightly longer than the 50 Export; length 29.3 mm; ID 14 mm; flame
shield and exhaust deflector; this apparently has a nozzle diameter of 0.030"
|
50C
|
Version sold by Sebel; differences from 50B
unknown
|
|
Sebel
|
|
Pressed
|
Looks identical to the 50B; we're still
investigating this model number; possibly this model has a larger nozzle diameter of
0.040"
|
Hell-Cat 50
|
|
|
|
|
|
Apparently identical to the 50B, except six
spring holes in cap; no flame shield but with exhaust deflector
|
The "original standard Jetex 50"
motor had a machined (turned) aluminum alloy case with "ribs," and a turned end cap
assembly. The "export model Jetex 50" and the Jetex 50B both used pressed
cases. Soon only the 50B model was made and sold, and the original models
dropped. The 50B has a slightly longer case, to increase the "free" combustion space
to give better wick-ejection properties.
The 50 Hell-Cat is the "standard"
size motor, "fitted with exhaust deflector ring to prevent damage to model through faulty
end cap sealing" (according to contemporary sales literature). Early models did not
have this deflector ring.
The 50 HT ("High Thrust") model
also holds two fuel pellets; for test runs or short flights you can use just a single
pellet, which, of course, cuts thrust duration in half. Fuel used in the standard and
HT engines is almost the same; the only difference is that HT fuel has a 1/8-inch [3.2 mm]
diameter hole through each pellet. It is ignited so that the fuel burns throughout
its entire length--not solely on the rear surface, as with the 50 Hellcat.
The 50 HT engine has a steel
chamber in place of the aluminum tube of the original Hellcat 50 engine, and is beefed up
in other ways as well. Combinations of fuel may be used in the HT 50 engine.
For example, you can use one HT pellet to give potent initial thrust and get a model off
the ground in a hurry, then in back of it put a Hellcat (standard Jetex 50) pellet, which
will give greatly increased thrust duration and much reduced push. There are many
tricks used to modify the Jetex engine thrust to suit specific models and conditions.
Historical
Notes
Jetex 50 was the third design
introduced, in 1949, by Wilmot & Mansour. It has also been produced in different
configurations by Sebel (UK) and Powermax.
Early after its introduction, the
Jetex 50 was somehow modified "for export," and subsequent (beginning about 1953) models
were packed as Jetex "50B" motors. The 50B version produced, according to Wilmot
& Mansour, "25% additional thrust."
We are not yet clear on the other
differences between these two models.
The current "50C" by Powermax
looks to us almost identical to the "50B" of Sebel; again we are not certain their
differences.
The 50 HT model was introduced
early in 1963; it was announced in American Modeler magazine, Mar-Apr 1963, p
21.
During a period when Jetex 50
motors were at peak popularity, an American firm designed a variation, sold widely as the
"Psst 50" and "Psst Double-50" motors. These are reviewed separately, as they have very different configuration
(but burn the same propellant).
In its current incarnations, the
50 is sold today in the models Jet-X 50C and 50Z, by Powermax. Powermax Jet-X sales
commenced in 1985.
Remarks
DO NOT confuse the 50
Hell-Cat (sometimes called the "50HC") with the very different 50 Rocket HT (a high-thrust
version, with a different nozzle). 50 Rocket HT propellant pellets are perforated
through their axis with a hole of about 1/8-in [3.2 mm] diameter. They must not be used in the smaller nozzled
50B, Hell-Cat, or similar motors!
Specific operational instructions
for the "Rocket HT" may be found on another
page.
Each engine takes two fuel
pellets; for test runs or short flights you can use just a single pellet, which, of course,
cuts thrust duration in half.
The Powermax Jet-X 50Z was
originally identical to the older Hell-Cat 50, with a larger nozzle diameter to accomodate
the higher burn rate and chamber pressures.
Suitable Model Aircraft
Wingspan (in)
[cm]
|
12-18 (20 with augmenter tube)
[30-46] [51 with augmenter tube]
|
Wing area (in²)
[cm²]
|
30-55
[194-355]
|
Weight (max, oz)
[gm]
|
0.75-2 (higher with augmenter
tube)¹
[21-57]
|
1. By some reports the 50-HT can lift a 2
ounce [57 gm] model "straight up."
Performance
Specifications
Data posted in green is from
original factory packaging and instruction sheets
Data in red indicates extrapolated
information, and must be regarded as approximate, at best
SI (metric) units
provided in brackets
Many weights and measures
courtesy David Fritchman, Socorro, NM
|
50
(Standard)
|
50
(Export) |
50B,
Hell-Cat, 50C¹
|
Rocket
50HT
|
50Z²
|
Thrust (avg, oz)
[gm]
|
0.5 [14]
(0.625 [18] with
later propellants, i.e. Red Spot)
|
0.5 [14]
(0.625 [18] with
later propellants, i.e. Red Spot)
|
0.6 [17]
(0.5 to 1.2 [14-34]
by some reports)
|
3.5-5.0 [99-142]
|
1.6 [45]
|
Thrust (max, oz)
[gm]
|
0.63 [17.9]
|
0.63 [17.9]
|
1.9 [54]
|
5.0 [142]
|
2.5 [71]
|
Thrust w/AT¹ (nom,
oz) [gm]
|
(not well suited for
augmentation, due to shape)
|
|
0.75 [21.3] (bellmouth only)
0.63 [17.9]
(short augmenter)
0.63 [17.9]
(long augmenter)
(by some
reports 1.0-0.8 [28-23] )
|
(perhaps not well suited for
augmentation, due to short burn time)
|
|
Duration
(sec/pellet)
|
14-15
|
10-12
|
10-12
|
|
~7
|
Duration (max,
sec)
|
14-15
|
10-12
|
15
12-16 (2 pellets)
20 (3 pellets)
|
3-5
|
20 (3 pellets)
25 (4 pellets)
|
Weight (dry, oz)
[gm]
|
0.25 [7.09]
|
0.2 [5.7]
|
0.2 [5.7]
0.3215 [9.11]
(see notes below) (0.219 to 0.282 [6.20-7.99] by some
reports)
|
0.375 [10.6]
|
0.353 [10.0]
|
Weight (full w/o
mount, oz) [gm]
|
0.36 [10.21]
|
0.30 [8.42]
|
0.4 [11.3]
(some reports say
0.33 to 0.4 [9.36 to 11.3] )
|
0.5 [14.2]
|
0.423 [12.25]
|
Propellant (min,
oz) [gm]
|
0.11 [3.10]
|
0.11 [3.10]
|
0.11 [3.10]
2.6 gm [1989]
|
|
2.2 gm [1989]
|
Propellant (max,
oz) [gm]
|
0.11 [3.10]
|
0.11 [3.10]
|
0.11
[3.10]
|
|
|
Total impulse
(oz-sec) [N]
|
7.0-7.5 [1.95-2.09]
|
5.0-6.0 [1.39-1.67]
|
6.0-7.2 [1.67-2.00]
|
|
|
Specific impulse
(Isp, sec)
|
64-68
|
45-55
|
55-65
|
|
|
Propellant mass
fraction²
|
0.69
|
0.67
|
0.50
|
|
|
Length (in)
[cm]
|
1.75 [4.45]
|
1.625 [4.13]
|
1.875 [4.8]
|
1.75 [4.45]
|
1.732 [4.4]
|
Width (max, in)
[cm]
|
0.688
[1.75]
|
0.625 [1.59]
|
0.625 [1.59]
|
0.75 [1.90]
|
0.708 [1.8]
|
Chamber ID (in)
[cm]
|
|
|
0.560 [1.42]
|
|
|
Throat (in)
[mm]
|
|
|
0.030-0.035 [0.76-0.89]
(0.03937 in = 1.0 mm in new models)
|
|
(0.03937 in = 1.0 mm)
|
Burn surface (nom,
in²) [cm²]
|
|
|
0.25 [1.59]
|
|
|
Operating pressure
(psia) [atm]
|
|
|
|
|
|
1: Weight aluminum engine mount, w/o supplied
screws: 0.04 oz [1.141 gm]. Case OD: 0.600 in [1.52 cm]. Case
length w/o nozzle: 1.225 in [3.11 cm] Case interior depth: 1.160 in [shoulder
to bottom of hemispherical end; 2.95 cm]. Nozzle length, shoulder to tip: 0.435
in [1.10 cm]
2: Has a much thicker and metal-reinforced
sealing washer (not suitable for any other engine), and a nozzle exhaust cone that are said
to increase the thrust by up to 25 percent. Uses perforated "Z" propellant pellets,
of which it can hold four. Minimum flights require two pellets. The motor is
gold anodized.
Additional
Illustrations
Jetex 50 (original issue)
This Wilmot Mansour original version of the Jetex
50 has a machined aluminum case and end cap, and shallow "ribs." (Graphics courtesy
Howard Metcalfe)
Jetex 50 Hellcat
Believed made by Sebel (UK); distributed by
Aristo-Craft Miniatures, NY; all steel, with aluminum motor mount. Single
spring. Note the forward end is hemispherically rounded. A blow-by ring is
tightly fitted over the chamber, and slid nearly to the aft end. This blow-by ring
was not present on some early Jetex 50 models, we think.
............
Jetex 50 Rocket HT
Left: a very early Rocket HT kit by American
Telasco. Right: Believed made by Sebel (UK); distributed by Aristo-Craft
Miniatures, NY; all steel, with aluminum motor mount.
The "HT" designation represents "high thrust." It has a rather high thrust of short
duration. Note twin closure springs to accommodate higher chamber pressure created by
perforated-grain pellets. Forward end of thrust chamber is generally flattened, with
a central dome perforated with a small machine screw, washers, and nut. The exact
purpose of this screw is unknown. Nozzle diameter is 1.5 mm, unlike the 50 Hellcat
and others in the series, which have a 1.0 mm diameter nozzle. Note also the absence
of a blow-by ring, as found on the Hell-Cat. If the chamber seal leaks, hot gas will
reverse direction, perhaps into or onto the model.
When the Rocket HT was
introduced, enthusiastic Jetex designers glowingly had this to say:
“New vistas of design are
opened up. Competition model aircraft should show tremendous improvements in
performance, attaining heights and flight-time averages heretofore impossible.
Space-type craft with stub wings for safe descent and landing will offer new
thrills. Scale ships such as the Lockheed F-104, and even the X-15, now are
feasible fliers. Scale Atlas, Thor, Titan and other full-scale boosters can be made
to lift off their pads and climb to exciting heights, all in complete safety. Who really
can say what ingenious modelers can do with a 500% increase in thrust? What way-out
designs will spring from the drawing boards? With the 50-HT to stir things up we
will not have to wait long to see.”
Specific operational instructions
for the "Rocket HT" may be found on another page.
...
Jetex 50 HT (top) beside Jetex
50 Hell-Cat (bottom)
In these views the differences can
be clearly seen, including the forward end shapes, with screw hole in the 50 HT.
...
Jetex 50 Hell-Cat (top, and right) beside an
early Jet-X 50Z (bottom, and left).
Looking carefully, one can see the difference in
shape of the nozzle closure stampings. The Hell-Cat is believed made by Sebel (UK),
while the Jet-X 50Z was made by Powermax more recently. Otherwise, the engines appear
identical, including the motor mount clips. Although the packaging for this "50Z"
engine is clearly marked, this engine appears to be identical to others currently sold as
Jet-X "50C" motors.
Jetex 50C, exploded view, showing
components.
1. Motor case
2. Exhaust deflector
ring
3. Solid fuel
pellets
4. Gauze disc
5. Igniter wick
6. Flame shield
7. Cap sealing
washer
8. Wire clip
9. End cap
.....
Jet-X 50C
Powermax motor, recent vintage. This is a
clean, sleek evolution from the original Wilmot Mansour Jetex 50 of 1949.
50Z
Powermax motor, recent vintage. Note the
exhaust nozzle, which may add some coefficient of thrust to the design. Exhaust
nozzle cones like this are essential parts of larger rocket engines, where they frequently
contribute an additional 150+% to the effective thrust.
|