G-Force-Moster_MacPara-Muse3

Inspection record for motorized paragliders
compatibility test
EAPR GmbH - Marktstr. 11 - D-87730 Bad Grönenbach - Germany
applicant
G-force Paramotors Raymond Ruckenstuhl
wing unit
Muse3 28
MTOW
135 kg
type test
number
EAPR-TW-7482/11
manufacturer
Mac Para
trimmer
ja
accelerator
ja
motor
Moster
EAPR-MS-7598/12
serial
number
nicht vorhanden
propeller
H30F 1,25m L-M-2
pitch
harness
G-Force
suspension
hoch am GZ, bewegl. Schubst.
maximum allowable total flying weight
test pilot
Anselm Rauh
test location
Tannheim
date
type test
number
serial
number
1328-1516
16°
135kg
20.09.2012
1. test of launch
special launch technique required
altitude gain after 300 meters > 15 meters
No
Yes
2. test of landing
special landing technique required
soft landing on pilots feet possible / soft landing on wheels possible (for paratrike)
No
Yes, by continuous braking
5. test of pitch stability and pitch damping and parachutal stall tendency when alternating between thrust and no thrust
turning from the axis of flight >15° after each change of load
No
canopy collapses
No
parachutal stall or stall is happening
No
pitch damping
pitch oscillations decreasing significantly
6. test of roll handling with thrust
horizontal figure "8" in less than 30 sec.
Yes
flat spin tendency
No
instable flight behavior, twist during change of direction
No
7. test of roll stability
behavior in roll movements and roll damping
rolling decreases significantly
8. test of roll stability in straight flight
rolling in straight flight
rolling >10° up to <15° but can be dampened by braking
Leichts Dauerrollen im Geradeausflug, leicht dämpfbar
9. test of spin tendency using minimal brake input
turning against the torque of the motor at 25% brake possible
yes, 180° in 10sec possible
10. test of stall at maximum motor thrust
brake travel in cm, braking force
tendency to enter parachutal stall
movement around yaw axis
>40cm, constant or increasing
No
<10°
11. test of recovery to normal flight from high angles of attack
followed by cascade
termination
No
yes, termination when thrust of motor is released
Dauersackflug unter Vollast möglich, bei Drosselung fährt der Schirm an
16 test of behavior of the paraglider in spiral dive
behavior of the paraglider when entering the manoeuvre
tendency to finish the turn and to return to level flight when exiting the
manoeuvre
paraglider increases bank angle and sink rate continuously with increasing pull on the brake line
bank angle stays the same, return to normal flight through slight pilot input (counter braking of the
outside half of the wing)
Bei geschlossenen Trimmern muss Spirale nach links aktiv beendet werden! (Kreuzgurt zum Drehmomentausgleich gespannt)
behavior of the paraglider when exiting the manoeuvre
paraglider returns to normal flight moderately after releasing the brakes. The resulting pendulum
movements do not require pilot input.
remarks
Leichte Trudelneigung beim Kurvenhandling mit viel Motorschub!
Abfluggewicht min. 125 kg
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Copyright Ralf Antz 2012
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