STRATOLAUNCH (roc)_20250225_082123_0000[1].pptx

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1. STRATOLAUNCH (roc)

2. INTRODUCTION The Stratolaunch Roc, also known as the Scaled Composites Model 351 Stratolaunch, it was introduced by the United States, It was announced in 2011, introduced in December 2011 .

3. Concept initiated by Paul Allen (co-founder of Microsoft) in 2011. eveloped by Scaled Composites (a subsidiary of Northrop Grumman). First flight on April 13, 2019. History & Development

4. Design & Specifications Twin-fuselage design, powered by six Pratt & Whitney PW4056 turbofan engines. Wingspan: 385 ft (117 m) – larger than any other aircraft. Length: 238 ft (73 m). Maximum takeoff weight: 1.3 million pounds (589,670 kg). Designed to carry rockets and hypersonic vehicles for mid-air launches.

5. 2019: First flight over Mojave Desert. 2022: Successful launch of Talon-A hypersonic test vehicle. Ongoing: Developing morehypersonic andspace -launch applications. The Stratolaunch achieved a top speed of 189 mph . Key Achievements

6. Weather-independent: Avoids delays from bad weather. Lower costs: More economical compared to traditional rocket launches. Greater flexibility: Launch from different locations . Advantages of Air Launching

7. Feature and Requirements The pilot, co-pilot and flight engineer are accommodated in the right fuselage cockpit. The flight data systems are in the left fuselage The Stratolaunch achieved a top speed of 189 mph It supported by 12 main landing gear wheels and two nose gear wheels, for a total of 28 wheels. The Stratolaunch Roc has six main fuel tanks and two auxiliary fuel tanks.

8. Conclusion Stratolaunch represents a new frontier in air-based space launches. Aims to revolutionize satellite deployment and hypersonic testing. Its continued development will shape the future of aerospace innovation .

9. cockpit of Stratolaunch (roc)

10. Thank you