OVERVIEW
The CASIC Sky Hawk represents a series of Unmanned Aerial Vehicle developments that includes the SH-1 and SH-3 forms.
The CASIC Sky Hawk represents a series of Unmanned Aerial Vehicle developments that includes the SH-1 and SH-3 forms.
YEAR: 2020
STATUS: In-Development
MANUFACTURER(S): China Aerospace Science and Industry Corporation (CASIC) - China
PRODUCTION: 1
OPERATORS: China (possible)
SPECIFICATIONS
Unless otherwise noted the presented statistics below pertain to the CASIC Sky Hawk 1 model. Common measurements, and their respective conversions, are shown when possible.
Unless otherwise noted the presented statistics below pertain to the CASIC Sky Hawk 1 model. Common measurements, and their respective conversions, are shown when possible.
CREW: 0
LENGTH: 7.55 feet (2.3 meters)
WIDTH: 13.78 feet (4.2 meters)
WEIGHT (EMPTY): 220 pounds (100 kilograms)
WEIGHT (MTOW): 331 pounds (150 kilograms)
ENGINE: 1 x Conventional engine driving two-bladed propeller in pusher configuration.
SPEED (MAX): 75 miles-per-hour (120 kilometers-per-hour; 65 knots)
RANGE: 186 miles (300 kilometers; 162 nautical miles)
CEILING: 16,404 feet (5,000 meters; 3.11 miles)
ARMAMENT
None. Mission-equipment carried.
None. Mission-equipment carried.
VARIANTS
Series Model Variants
• Sky Hawk - Base Project Name.
• Sky Hawk 1 (SH-1) - Model of 2008; miniature UAV form; catapult-launched; flying wing fuselage; conventional engine driving two-bladed propeller unit in pusher configuration.
• Sky Hawk 3 (SH-3) - Twin-boom fuselage configuration; conventional engine driving two-bladed propeller unit in pusher configuration; inverted-V tailplanes; skid undercarriage.
• Sky Hawk 3A (SH-3A) - Based in the SH-3 form; tricycle undercarriage; increased MTOW.
• Sky Hawk 3B (SH-3B) - Micro-Air Vehicle (MAV) form; revised, traditional fuselage layout; electrically-driven.
Series Model Variants
• Sky Hawk - Base Project Name.
• Sky Hawk 1 (SH-1) - Model of 2008; miniature UAV form; catapult-launched; flying wing fuselage; conventional engine driving two-bladed propeller unit in pusher configuration.
• Sky Hawk 3 (SH-3) - Twin-boom fuselage configuration; conventional engine driving two-bladed propeller unit in pusher configuration; inverted-V tailplanes; skid undercarriage.
• Sky Hawk 3A (SH-3A) - Based in the SH-3 form; tricycle undercarriage; increased MTOW.
• Sky Hawk 3B (SH-3B) - Micro-Air Vehicle (MAV) form; revised, traditional fuselage layout; electrically-driven.
HISTORY
Detailing the development and operational history of the CASIC Sky Hawk Unmanned Aerial Vehicle (UAV). Entry last updated on 11/9/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
Detailing the development and operational history of the CASIC Sky Hawk Unmanned Aerial Vehicle (UAV). Entry last updated on 11/9/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The CASIC "Sky Hawk" of Chinese aero-industry encompasses a family of related Unmanned Aircraft Systems (UASs) for both military and commercial service. These include the Sky Hawk 1 and Sky Hawk 3 lines. A new, 6,600lb all-wing design was showcased by the company at Zhuhai Air Show 2018 (and slated for the stealth surveillance role), further expanding on the current family offerings.
CASIC stands for "China Aerospace Science and Industry Corporation".
The first entry, the Miniature-UAV "SH-1", was revealed at Zhuhai Air Show 2008 as an all-wing design driven by a two-bladed conventional engine arranged in "pusher" configuration. The overall arrangement of the fuselage is more traditional than the SH-3 version detailed below. Its payload capacity reaches 66lb and launching of this vehicle is by rocket-assisted, catapult action while recovery is through simple released parachute to retard the fall. Skids make up the undercarriage facilities. Its overall length reaches 7.5 feet with a wingspan covering 13.78 feet. It can reach speeds around 90 mph up to a ceiling of 16,400 feet.
The SH-3 switches to a twin-boom fuselage arrangement with a similar pusher engine configuration as the SH-1. However, the tail section introduces a pair of downward-facing, outward-canted vertical planes for stability though recovery is similar to the SH-1 involving parachute and skid formation. Its length is increased out to 11.8 feet while its wingspan equals this measurement. The payload capacity is a relatively restricted 11lb. The operating ceiling of this entry is reduced to 9,840 feet while operating at speeds nearing 75 mph.
The SH-3 model includes both the "SH-3A" and "SH-3B" models. The A-model introduces a more conventional wheeled tricycle undercarriage for improved runway/airfield support (no longer requiring the use of a catapult for launching) though recovery still involves parachute deployment. The B-model is a very different hand-launched Micro-Air Vehicle (MAV) approach - though still powered by a twin-bladed pusher propeller unit which is electrically-driven in the design. Flight time is limited to 45 minutes and recovery is by runaway/airfield or parachute fall.
CASIC stands for "China Aerospace Science and Industry Corporation".
The first entry, the Miniature-UAV "SH-1", was revealed at Zhuhai Air Show 2008 as an all-wing design driven by a two-bladed conventional engine arranged in "pusher" configuration. The overall arrangement of the fuselage is more traditional than the SH-3 version detailed below. Its payload capacity reaches 66lb and launching of this vehicle is by rocket-assisted, catapult action while recovery is through simple released parachute to retard the fall. Skids make up the undercarriage facilities. Its overall length reaches 7.5 feet with a wingspan covering 13.78 feet. It can reach speeds around 90 mph up to a ceiling of 16,400 feet.
The SH-3 switches to a twin-boom fuselage arrangement with a similar pusher engine configuration as the SH-1. However, the tail section introduces a pair of downward-facing, outward-canted vertical planes for stability though recovery is similar to the SH-1 involving parachute and skid formation. Its length is increased out to 11.8 feet while its wingspan equals this measurement. The payload capacity is a relatively restricted 11lb. The operating ceiling of this entry is reduced to 9,840 feet while operating at speeds nearing 75 mph.
The SH-3 model includes both the "SH-3A" and "SH-3B" models. The A-model introduces a more conventional wheeled tricycle undercarriage for improved runway/airfield support (no longer requiring the use of a catapult for launching) though recovery still involves parachute deployment. The B-model is a very different hand-launched Micro-Air Vehicle (MAV) approach - though still powered by a twin-bladed pusher propeller unit which is electrically-driven in the design. Flight time is limited to 45 minutes and recovery is by runaway/airfield or parachute fall.
MEDIA
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed Rating
Hi: 100mph
Lo: 50mph
This entry's maximum listed speed (75mph).
Graph average of 75 miles-per-hour.
City-to-City Ranges
NYC
LDN
LDN
PAR
PAR
BER
BER
MSK
MSK
TKY
TKY
SYD
SYD
LAX
LAX
NYC
Graph showcases the CASIC Sky Hawk 1's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
1
1
Altitude Visualization
