The secret is in two details: how SpaceX engineers do the impossible

SpaceX has become one of the most innovative and influential players in the modern aerospace industry. Founded by Elon Musk to make space travel more affordable and ultimately contribute to the colonization of Mars, SpaceX has repeatedly demonstrated its willingness to challenge traditional aerospace norms. From the development of reusable rocket stages to a flexible organizational structure, the company has redefined what it means to be competitive in an industry once dominated by long-standing giants.

In this article, we will examine the starting point of creating a new high-tech product, analyze how SpaceX realizes the integration of new technologies in a very short time, and explain what exactly allows SpaceX engineers to do the impossible.

Factors that determine the championship

Cost efficiency. Thanks to frequent launches, reuse, and vertical integration, SpaceX has reduced overall mission costs and optimized production processes. A typical example of the cost-effectiveness and innovation that SpaceX combines is the ability of its engineers to produce an assembly node at a cost ten times cheaper than third-party manufacturers. This saves hundreds of thousands of dollars on the development of individual parts. This is the result of the management’s long-term planning and willingness to invest in expanding its production and capacity. One example of this is the development and implementation of a friction welding machine to work with complex multi-level structural parts of rockets. While other aerospace companies shy away from such procedures, the development of this machine has allowed SpaceX to reduce excessive stress on the structure of its rockets and optimize efficiency.

Reliability and performance. With an extensive track record of successful missions and continuous improvements to rocket systems, SpaceX maintains high reliability and consistent performance during each launch.

Organization of the microclimate in the company. A culture of innovation with an emphasis on rapid iteration, continuous product improvement, an openness to risk and a “fail fast, learn faster” philosophy helps the RnD team push the boundaries of design. Complementing this, the compact operating structure enables rapid decision-making through a flat hierarchy, minimizing bureaucracy to meet project schedules. SpaceX views risks as learning opportunities and experiences. Developers actively analyze technical errors identified during a failed test and take preventive measures to correct them. This spirit and culture overcome the fear associated with working on risky projects.

Technological innovations. The company has done a titanic job in developing aerodynamic and strength analysis of its systems. For applied engineers and scientists, SpaceX stands out primarily for its advanced approach to aerodynamic and strength analysis. Using state-of-the-art computational fluid dynamics (CFD), the company refines every contour of its rocket structures to minimize drag and optimize stability. In addition, rigorous structural testing ensures that critical components can withstand extreme operational loads with a minimum guaranteed safety margin. This robust symbiosis between aerodynamic modeling and strength analysis is the foundation of SpaceX’s technological advantage, enabling the creation of high-performance designs.

Integration: from idea to product

SpaceX is currently improving the Starship launch vehicle, which should allow for the transportation of humans to Mars in the near future. Let’s look at what features of the SpaceX engineering team’s design approach make the introduction of new technologies fast and high-quality for the company, using the example of the Starship’s conversion to Hot Stage Separation technology*.

*Hot Stage Separation is a method of separating the stages of a multi-stage rocket in which the engine of the next stage is started before the previous stage is separated. This approach, also known as “Fire-In-The-Hole” (FITH), reduces the pause between the shutdown of one stage and the launch of another, providing continuous thrust and increasing flight efficiency.

Head Stage Separation technologies (HST) methods and systems rely on flow modeling analysis to predict pressure gradients, thermal loads, and gas expansion when the second stage engine ignites before the first stage shuts down completely. CEAS Space Journal has an interesting article from Ukrainian experts about a new perspective on this process.

Positive advantages of the hot stage separation method

  • Improved traction efficiency
  • Reducing the time to complete a mission
  • Reduced interruption of aerodynamic flow
  • Simplifying the coordination of the stages
  • Potential increase in payload capacity
  • Improved reuse strategies

The main challenges for the engineering team when integrating hot stage separation

  • A ship with a height of ~50 m performs asymmetric maneuvers
  • The engines are started in a confined space
  • Shielding in the intermediate stage is required to reuse the first stage of the booster
  • Interstage vent design
  • Sophisticated and complex computing

To integrate the system, two key elements had to be analyzed and designed: the Grid Fins and the Interstage Vent. The former provides the necessary flight control and stability of the booster during and after hot stage separation, while the interstage vents prevent potentially harmful pressure imbalances. Both aspects are indispensable to make hot stage separation feasible and reliable.

Starship with interstage vents (a) and grid fins (b) section installed

Why are these elements so important?

  1. Controlling complex aerodynamics with grid fins

Control after separation. When the second stage is ignited and the parts separate under the influence of thrust, the first stage (booster) requires precise control surfaces to maintain a stable flight. The grid provides high control accuracy during the initial reorientation of the launch vehicle and subsequent return to the launch site or landing maneuvers.

Mitigating the impact of exhaust gases. When using FITH, the flame and second-stage plume may briefly interact with the aft portion of the booster. The grid ribs must be designed and analyzed to handle the altered flow conditions, including turbulent wake zones and potential collision with the plume.

Quick correction. At the moment of separation, the forces acting on the booster can suddenly change. The grids, in combination with the booster motors, compensate for these changes in forces, helping the vehicle to stabilize immediately after it is disengaged from the second stage.

  1. Ensure proper pressure equalization using an interstage vent

Preventing pressure build-up. In the case of a hot split, the ignition of the second stage causes a sudden increase in pressure and temperature around the interstage area. Carefully designed ventilation paths prevent dangerous overpressures that could damage the booster or the second stage.

Protecting structural integrity. If pressure drops are not controlled, you may experience structural stresses on the interstage walls or unwanted aerodynamic loads. Proper ventilation ensures that gases can escape safely, reducing the chance of structural failure during separation.

Avoiding flow disturbances. Vent analysis also helps control the direction and velocity of exhaust gas flow, minimizing any unexpected aerodynamic interactions. This control is essential for clean separation, preventing re-contact or other anomalies.

By understanding SpaceX’s basic principles, key success factors, the intricacies of its approach to integrating parts, and the critical function of grid fins and interstage vent, we have established a solid foundation for understanding the company’s overall approach and strategy. In the next installment, we’ll turn our attention to in-depth technical analysis, exploring how advanced aerodynamic analysis and creative approache to dry-calculations drive Starship’s cutting-edge performance.

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