SpaceX’s Starship Refuelling Solution: Nova Starship! скачать в хорошем качестве

SpaceX’s Starship Refuelling Solution: Nova Starship!

SpaceX’s Starship Refuelling Solution: Nova Starship! === #space #spacezone #starship === SpaceX’s Starship Refuelling Solution: Nova Starship! For Starship to reach the Moon, in-orbit refueling is essential. This is one of Starship's biggest challenges. So, what if it wasn’t? This is the solution to send humans back to the Moon without orbit refueling. Well, before we explore how Starship might achieve this, we need to take a step back and uncover the story of a forgotten rocket. Long before the mighty Saturn V took shape—and back when it was still called the Juno V—NASA had its sights set even higher. In the 1950s, the U.S. Air Force began developing a powerful new engine, the F-1, capable of producing a staggering 1.5 million pounds of thrust. When NASA was established in 1958, the agency began envisioning a launch vehicle that could go beyond Earth orbit—one that could carry astronauts all the way to the Moon. SpaceX’s Starship Refuelling Solution: Nova Starship! This ambitious concept became known as Nova. It was the centerpiece of NASA's first long-range plan, which outlined a vision for human space exploration and was presented to President Eisenhower on January 27, 1959. Nova had a simple mission: to enable a direct ascent approach to lunar exploration. This meant landing a spacecraft on the lunar surface in one continuous flight—without assembling components in Earth orbit or relying on a separate lander waiting in lunar orbit. It was a bold, all-in-one approach to reaching another world. SpaceX’s Starship Refuelling Solution: Nova Starship! To achieve this, the rocket was engineered to be an absolute powerhouse. The first stage was an enlarged version of the S-IC, equipped with eight F-1 engines delivering a staggering 61,925 kN of thrust. The second stage followed suit, based on a widened S-II design and powered by eight J-2 engines generating 8,265 kN of thrust. The third stage was a stretched version of the S-IVB, maintaining its original diameter and engine configuration to complete the mission.