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    SM-28T Machete LC Uae 2022

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    Stavatti
    SM-28T Machete Linecard in a hypothetical UAE livery. The SM-28T is a two seat tandem, next generation non-afterburning turbofan powered subsonic Attack and Close Air Support (CAS) aircraft now under development by Stavatti Aerospace Ltd.

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    SM-28T Machete LC Uae 2022

    Uploaded by

    Stavatti
    45 views2 pages
    SM-28T Machete Linecard in a hypothetical UAE livery. The SM-28T is a two seat tandem, next generation non-afterburning turbofan powered subsonic Attack and Close Air Support (CAS) aircraft now under development by Stavatti Aerospace Ltd.

    Original Title

    SM-28T_MACHETE_LC_UAE_2022

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    © © All Rights Reserved

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    SM-28T Machete Linecard in a hypothetical UAE livery. The SM-28T is a two seat tandem, next generation non-afterburning turbofan powered subsonic Attack and Close Air Support (CAS) aircraft now under development by Stavatti Aerospace Ltd.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    45 views2 pages

    SM-28T Machete LC Uae 2022

    Uploaded by

    Stavatti
    SM-28T Machete Linecard in a hypothetical UAE livery. The SM-28T is a two seat tandem, next generation non-afterburning turbofan powered subsonic Attack and Close Air Support (CAS) aircraft now under development by Stavatti Aerospace Ltd.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    of 2

    STAVATTI AEROSPACE • 9400 Porter Road, Niagara Falls, NY 14304 USA • TEL: (651) 238-5369 • email: machete@stavatti.com • http://www.stavatti.

    com
    Performance &
    TURBOFAN MACHETE
    Specifications
    FLYAWAY COST: $20 Million AVAILABILITY: TBD

    TYPE

    Two Seat Close Air Support (CAS), Anti-Armor/Maritime Strike (AA/MS) and Advanced Trainer Aircraft (AT)

    ACCOMMODATION

    Flight Crew of Two Seated in Tandem on Martin Baker MK16E or MK18 Zero-Zero Ejection Seats

    POWERPLANT

    One (1) General Electric Aircraft Engines Non-Afterburning F414 Derivative Turbofan Delivering 14,756 lb st.

    STRUCTURE

    Cantelever three spar semi-monocoque titanium foam metal sandwich wing, canard and empennage with modular
    four element semi-monocoque titanium and aluminum foam metal sandwich fuselage.

    ARMAMENT

    One Ventral Centerline Mounted General Dynamics Four Barrel GAU-13/A 30mm Gatling Cannon with 600 rds;
    Eight Underwing Stores Pylons with 14-in Suspension for a Maximum External Warload of 12,000 lbs.

    DIMENSIONS

    Wingspan 53 ft 0 in Wing Area 354 sq ft


    Length Overall 38 ft 6 in Wheelbase 16 ft 2 in
    Height Overall 12 ft 11 in Wheeltrack 12 ft 1 in

    WEIGHTS & CAPACITIES LOADINGS

    Empty Weight 16,400 lbs Wing Loading @ TCW (lbs/sq ft) 75.7
    Maximum Internal Fuel (IF) 6,000 lbs Thrust-to-Weight @ TCW 0.55
    Max External Load/Warload 12,000 lbs Wing Loading @ MTOW (lbs/sq ft) 101.7
    Typical Combat Weight (TCW) 26,800 lbs Thrust-to-Weight @ MTOW 0.41
    Max Take-Off Weight (MTOW) 36,000 lbs Positive Load Limit @ MTOW 7.5

    PERFORMANCE

    Max Level Speed @ SL 0.90 Mach Max Range, 0.90 M/FL 150, IF 487 nm
    Max Level Speed @ 15,000 ft 0.90 Mach Max Range, 0.90 M/FL 350, IF 1,067 nm
    Max Level Speed @ 35,000 ft 0.90 Mach Cruise Range, 0.85 M/FL 150, IF 662 nm
    Max Cruise Speed @ 15,000 ft 0.85 Mach Cruise Range, 0.85 M/FL 350, IF 1,394 nm
    Max Cruise Speed @ 35,000 ft 0.85 Mach Cruise Range, 0.80 M/FL 150, IF 760 nm
    Typical Cruise @ 25,000 ft 0.80 Mach Cruise Range, 0.80 M/FL 350, IF 1,537 nm
    Typical Cruise @ 35,000 ft 0.80 Mach Ferry Range with 2 x 150 USG Tanks 3,830 nm
    Typical Approach Speed @ SL 94 KTAS Takeoff Ground Roll, Takeoff Weight 1,765 ft
    Typical Landing Stall Speed @ SL 79 KTAS Landing Ground Roll, Landing Weight 2,063 ft
    Max Initial Rate-of Climb @ SL 17,000 ft/min Service Ceiling Exceeds 55,000 ft

    RELEASE: MAY 2022 COPYRIGHT © 2022 STAVATTI AEROSPACE LTD

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