Single engine piston aircraft with fixed landing gear. The M-5-210C Lunar Rocket seats up to 3 passengers plus 1 pilot.

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Performance specifications

Horsepower:

1 x 210 HP

Best Cruise Speed:

126 KIAS

Best Range (i):

410 NM

Fuel Burn @ 75%:

10.0 GPH

Stall Speed:

33 KIAS

Rate of climb:

1,250 FPM

Ceiling:

18,000 FT

Takeoff distance:

150 FT

Landing distance:

200 FT

Takeoff distance over 50ft obstacle:

600 FT

Landing distance over 50ft obstacle:

600 FT

Weights

Gross Weight:

2,300 LBS

Empty Weight:

1,350 LBS

Fuel capacity:

40 GAL

Ownership Costs 1974

Total Cost of Ownership:

$19,618.31

Total Fixed Cost

$6,796.71

Annual inspection cost:

$1,221.00

Storage:

$840.00

Weather service:

$604.89

Insurance:

$1,675.47

Refurbishing and modernization:

$364.42

Depreciation:

$2,090.93

Total Variable Cost (127.0 Hrs)
Cost Per Hour = $100.96
Cost Per Mile = $0.80

$12,821.60

Fuel cost per hour:
(10.0 gallons/hr @ $5.40/gal)

$54.00

Oil cost per hour:

$3.35

Overhaul reserves:

$15.29

Hourly maintenance:

$18.31

Misc: landing, parking, supplies,
catering, etc

$10.00

Engine (x1)

Manufacturer:

Cont Motor

Model:

IO-360-D

Horsepower:

210 HP

Overhaul (HT):

1,500 Hrs

Years before overhaul:

12