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    • Home
    • About Us
    • Services
    • Expertise
      • Aeronautical Research
      • Astronautical Research
      • Education & Training
      • Technology Team
    • Research
      • Publications
      • Hypersonic Vehicle Patent
      • Rocket-Ramjet Patent
    • Blog
    • Media
    • Contact Us
  • Home
  • About Us
  • Services
  • Expertise
    • Aeronautical Research
    • Astronautical Research
    • Education & Training
    • Technology Team
  • Research
    • Publications
    • Hypersonic Vehicle Patent
    • Rocket-Ramjet Patent
  • Blog
  • Media
  • Contact Us

Founder & CEO: Engr. Dr. Ali Sarosh

Our Founder & CEO

  Engr. Prof. Dr. Ali Sarosh is a senior aerospace executive, technology strategist, and the Founder and Chief Executive Officer of Shocks & Stars Engineering. With over 30 years of leadership experience spanning defense, advanced aerospace research and development, and corporate innovation, Dr. Sarosh drives the company's strategic vision to deliver viable, cost-effective solutions for low-cost space access, space debris remediation, and hypersonic propulsion.

  

Corporate Leadership & Strategic Vision

At Shocks & Stars, Dr. Sarosh has established agile research ecosystems—including the AstroFlux and AeroFlux laboratories—to bridge the gap between theoretical research and commercial aerospace applications. Under his executive direction, the technology startup secured a decisive victory in Cohort-1 of the National Incubation Center for Aerospace Technologies (NICAT) for the AstroFlux space debris remediation mission. He has successfully positioned the company as a key player in the commercial aerospace sector by acquiring national design projects for hypersonic space transportation and forging international partnership agreements to design space propulsion units for commercial satellites. 

  

 

Executive Highlights & Industry Impact

  • Executive R&D Management: Secured and directed over PKR 11.06 million in competitive funding as Principal Investigator, leading national-scale aerospace technology development programs for organizations such as NESCOM, SUPARCO, and the Pakistan Air Force
  • Defense & Aviation Leadership: Completed a distinguished three-decade career in the Pakistan Air Force, retiring as a Group Captain, and served as Deputy Chief Engineer of Technology at the Aircraft Manufacturing Factory (PAC Kamra)
  • Global Engineering Collaborations: Led high-stakes international joint development programs, including technology leadership for the JF-17 Thunder aircraft in China and design engineering for the Super Mushshak-III in Sweden and Saudi Arabia
  • National Space Strategy: Serves as a Technical Advisor to the Ministry of Science and Technology (MoST) for the establishment of the Pakistan Space Centre (PSC) and has represented Pakistan's space transportation interests at the UN UNOOSA-ICAO Forum in Vienna
  • Innovation & Intellectual Property: Holds awarded design patents for rocket-ramjet integrated systems and hypersonic space transportation configurations, bringing a deep technical foundation to executive decision-making
  • Honors & Global Affiliations: Honored with the Presidential Imtiazi Sanad by the Government of Pakistan for establishing indigenous space capabilities, and serves as a Senior Member of the American Institute of Aeronautics and Astronautics (AIAA). 

 

Technological Expertise & Academic Foundations

  • Specialized Domain Knowledge: Expert in hypersonic flight systems, advanced combined-cycle propulsion (Scramjet, RBCC), and dual-use space technologies
  • R&D Translation: Focuses on translating advanced academic research into viable engineering solutions, advising on space security, non-proliferation, and sustainable space architectures
  • Academic Pedigree: Holds a PhD in Space Launch Vehicle Design and an MS in Aerospace Propulsion from Beihang University (China), alongside a BE in Aerospace Engineering from NED University; actively cultivates the next generation of aerospace talent as an Associate Professor at Air University, Islamabad. 

Learn More

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Find out more

Feasibility assessment of running JP-8 fuel in diesel engine

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A novel KFCM based fault diagnosis method for unknown faults in satellite reaction wheels

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Artificial Bee Colony algorithm for parametric optimization of spacecraft attitude tracking control

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An Aerothermodynamic and Mass-Model Integrated Optimization Framework for Highly-Integrated Forebody

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STS forebody material selection method using integrated aerothermodynamic optimization approach

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Policy Considerations for Nascent Space Powers

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A Cognitive-Heuristic Framework for Optimization of Spaceplane-System Configurations

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Heuristic-intelligent design schemes a solution paradigm for transatmospheric cruiser

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Nascent Space Powers: Some Policy Issues

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Hybrid Assisted Regenerative Turbofan Engine: A case study for XWB-84 Modification

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Space Technology Applications for Maritime Intelligence, Surveillance, and Reconnaissance

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Integration of small telescopes with satellite tracking analytical model for space situational aware

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A Computationally Intelligent Expert System for Design Parameterization of Sub-Orbital Carrier

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A TIPSO-SVM Expert System for Efficient Classification of TSTO Surrogates

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An Aerothermodynamic Design Approach for Scramjet Combustors and Comparative Performance...

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An Aerothermodynamic-CFD Approach for Design of Hydrogen-Fuelled, Constant-Area Scramjet Combustor

For more information on the mentioned research paper, please: 

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Wake reduction in horizontal axis wind turbine: A review of advancements in techniques

For more information on the mentioned research paper, please: 

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A FOM Based Computational Heat Transfer Method for Aerothermal Analysis of Airborne Electronics LRU

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Wake reduction in horizontal axis wind turbine: A review of advancements in techniques

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Mechanical Components Design for a HARTFE Configuration for Future Aircraft propulsion

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Design of Rocket-Ramjet Integrated System

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Design of Hypersonic Space Transportation System

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Erratum to: A Cognitive-Heuristic Framework for Optimization of Spaceplane-System Configurations

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Modal Analysis of Thin Walled Multi-cell Composite Doubly Tapered Beams of Closed Cross Sections

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An Integrated Design and Intelligent Optimization Framework for Forebody-Inlet Configuration...

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An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent mod

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Structural optimization of elliptical-tip star propellant grain using sub-problem approximation

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Study of Design and Performance Analysis for Comparative Hydrogen-Fuelled Scramjet Propulsion System

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Modal Analysis of Thin Walled Multi-cell Composite Doubly Tapered Beams of Closed Cross Sections

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Robotic Manipulator for Space Debris Mitigation in Low Earth Orbit

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A NOVEL TWO-STEPS PSO ALGORITHM SOLUTION FOR AEROTHERMODYNAMIC OPTIMIZATION PROBLEM

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Parametric Simulations of Dilution of Position (DOP) and Navigation Accuracy Using Satellite Toolkit

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International Journal of Mechanical, Industrial and Aerospace Sciences

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Heuristic-Intelligent Design Schemes

Customers have questions, you have answers. Display the most frequently asked questions, so everybody benefits.

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Conceptual design of independently configurable Mach 6.8 hydrogen fuelled dual mode scramjet

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A Survey of Research Advancement on Unstart Flow Mechanism of The Air-Breathing Hypersonic Inlet

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