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Jetex 35 motor

General Description

This is the smallest and lightest of the Jetex units, with a nominal or rated thrust output of 3/8 to 1/2 ounce [11-14 gm].  It has one or two different features compared with older Jetex units.

Apparently at least two different 35 series motors have been sold, of which we have little information yet.  If you can share a photo, drawing, scan, or whatever, please let us know so we can post them here.

The Powermax Jet-X 35 engine can hold up to four propellant pellets.

Historical Notes

Also originally designed by Wilmot and Mansour, and introduced in the September 1953 issue of Aeromodeller magazine (p 517).  An earlier mention of this engine is also in the August 1953 issue, under the Gregory's ad.

Remarks

This is the smallest Jetex built.  It is generally shaped like the Jetex 50, being made of a pressed metal case. Only one pellet can be loaded.  The external shape of the end cap makes it suitable for use with an augmenter tube.

Unlike other motors, the Atom 35 has a tapered combustion hamber leading to the actual jet nozzle, and a cone shaped washer in the end of the case, called a "bottom shield."  The Jetex 35 fuel pellets have a special coned recess (some call it a "hollowed charge") to fit this.  These pellets produce considerably reduced power for the last 2-3 seconds of burn, to assist the power-to-glide transition.  Most Jetex engines have a surge of thrust toward the end of the charge duration.  (This is opposite the Scorpion engine's pellet loading, where the hollow end is inserted last.)

Pellet charges for the 35 may be found to be quite a tight fit in the case, calling for adequate cleaning out each time to avoid the fresh charge jamming.

Suitable Model Aircraft

Wingspan (in)
[cm]
10 to 12
[25-30]
Wing area (in²)
[cm²]
25 to 40
[161-258]
Weight (max, oz)
[gm]
0.62 to 0.75
[18-21]
(1.0 with some airplane models)
[28 with some airplane models]

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

Jetex Atom 35
Jet-X 35 (Powermax)
Thrust (avg, oz) [gm]
0.4 [11.3]
(0.375-0.50)
[10.6-14]
2.5 [70.9]
Thrust (max, oz) [gm]
0.5 [14.18]
 
Thrust w/AT¹ (nom, oz) [gm]
0.5 [14]
 
Duration (sec/pellet)
 7-9
(8-10 with later formulations)
 
Duration (max, sec)
12
(8-10 with later formulations)
 
Weight (dry, oz) [gm]
0.15 [4.25]
(0.156) [4.43]
0.106 [3.00]
Weight (full, oz) [gm]
0.3 [8.50]
 
Propellant (min, oz) [gm]
0.094 [2.66]
 
Propellant (max, oz) [gm]
0.094 [2.66]
 
Total impulse (oz-sec) [N]
2.8-3.6 [0.78-1.00]
 
Specific impulse (Isp, sec)
 29-38
 
Propellant mass fraction²
0.50
 
Length (in) [cm]
1.6 [4.0]
(1.625) [4.13]
1.732 [4.40]
Width (max, in) [cm]
 0.6 [1.52]
 
Chamber ID (in) [cm]
 
 
Throat (in) [mm]
 
 
Burn surface (nom, in²) [cm²]
 
 
Operating pressure (psia) [atm]
 
 

Additional Illustrations

Jetex 35 Engine
Jetex 35 engine, with screen, fuel pellet, and "dimpled" bottom shield that fits pellet

Jetex 35 with fuel pellet
Jetex 35 engine, showing "dimpled" fuel pellet and correct installation


Early Jetex 35 fuel pellets kit, imported by American Telasco


Jetex 35 disassembled


Jet-X 35 of modern vintage, by Powermax (UK)

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Operations  | Propellants  | Individual Motors
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