Space technology
Space technology encompasses the engineering disciplines, tools, and systems developed to facilitate human activities beyond Earth's atmosphere, including spacecraft design, propulsion, life support, and communication infrastructure for exploration, satellite operations, and scientific research.[1] Defined as technologies supporting operations above the Kármán line—approximately 100 kilometers (62 miles) above sea level—it enables both crewed missions, such as those to the International Space Station, and uncrewed endeavors like deep space probes and Earth-orbiting satellites.[2] The origins of space technology trace back to early 20th-century rocketry experiments, but it emerged as a distinct field in the late 1950s amid Cold War competition. On October 4, 1957, the Soviet Union launched Sputnik 1, the first artificial satellite, which orbited Earth and transmitted radio signals, marking the onset of the Space Age and demonstrating practical rocketry for space access.[3] This spurred the United States to establish NASA in 1958 and accelerate developments, leading to milestones like the first human spaceflight by Yuri Gagarin in 1961 and the Apollo program's six successful Moon landings from 1969 to 1972, which advanced propulsion, guidance, and life support systems. By the early 1980s, reusable launch vehicles like the Space Shuttle had been introduced to improve efficiency and reduce costs, while international collaboration culminated in the International Space Station (ISS), operational since 1998 as a platform for long-duration human presence in space.[4] In the 21st century, space technology has expanded dramatically, driven by commercialization and miniaturization. As of November 2025, approximately 13,500 active satellites orbit Earth, supporting global telecommunications, GPS navigation, and environmental monitoring, though this proliferation has increased the total number of tracked objects, including debris, to over 45,000.[5][6] Key components include launch vehicles for orbital insertion, in-space propulsion systems (chemical, electric, and emerging propellantless types), spacecraft subsystems for power, thermal control, and avionics, and ground-based networks for data handling.[7] The rise of the "NewSpace" economy, led by private entities, has lowered launch costs through reusable rockets and enabled small satellite constellations like Starlink, while initiatives such as NASA's Artemis program target sustained lunar exploration and preparation for Mars missions.[2] These advancements not only push the boundaries of scientific discovery but also yield Earth-based benefits, including improved weather forecasting and disaster response technologies.[8]Fundamentals
Basic Principles
Space technology relies on fundamental principles of physics and engineering to enable operations beyond Earth's atmosphere. Newton's laws of motion provide the core framework for understanding spacecraft behavior in space. The first law states that an object remains at rest or in uniform motion unless acted upon by an external force, explaining why satellites maintain orbit without continuous propulsion once inserted. The second law, F = ma, relates thrust to acceleration, guiding the design of propulsion systems to achieve necessary velocities. The third law, action-reaction, underpins rocket propulsion, where expelling exhaust gases propels the vehicle forward.[9] To escape a celestial body's gravitational pull, such as Earth's, a spacecraft must attain escape velocity, the minimum speed required to reach infinity without further propulsion. This is derived from conservation of energy and given by the formulav = \sqrt{\frac{2GM}{r}}
where G is the gravitational constant ($6.67430 \times 10^{-11} \, \mathrm{m^3 \, kg^{-1} \, s^{-2}}), M is the mass of the central body (for Earth, $5.972 \times 10^{24} \, \mathrm{kg}), and r is the distance from the body's center (Earth's radius is approximately $6,371 \, \mathrm{km}). For Earth at the surface, this yields about 11.2 km/s. Orbital mechanics governs how objects move under gravity, building on Newton's law of universal gravitation. Kepler's three laws describe planetary and satellite motion: (1) orbits are ellipses with the central body at one focus; (2) a line from the body to the orbiting object sweeps equal areas in equal times, implying varying speed; (3) the square of the orbital period T is proportional to the cube of the semi-major axis a, or T^2 \propto a^3. These laws apply to artificial satellites as well. Common orbit types include low Earth orbit (LEO) at altitudes of 160–2,000 km, with periods around 90 minutes, used for Earth observation; and geostationary orbit (GEO) at 35,786 km altitude, with a 24-hour period matching Earth's rotation, allowing fixed positioning over a point. To change orbits efficiently, the Hohmann transfer uses an elliptical path tangent to both initial and target circular orbits, requiring two impulsive burns: one to enter the transfer and one to circularize at the destination.[10][11][12] The space environment imposes unique challenges due to its near-vacuum conditions, thermal extremes, and microgravity. In the vacuum of space near Earth, pressure is approximately $10^{-6} Pa, far below atmospheric levels, leading to outgassing where volatile materials in spacecraft components sublimate or evaporate, potentially contaminating optics or altering surfaces. Thermal extremes arise from direct exposure to solar radiation without atmospheric buffering; at 1 AU from the Sun, the solar flux, known as the solar constant, is about 1,366 W/m², causing temperatures to fluctuate from -150°C in shadow to +120°C in sunlight, stressing materials through expansion and contraction. Microgravity, effectively weightlessness, affects fluid behavior and material processing, such as preventing bubbles from rising in liquids during manufacturing or causing uneven sedimentation in experiments, which must be mitigated through design or active control.[13][14][15]