OrbitalHub

Wikipedia dicit:

Starship is a fully-reusable and super heavy-lift launch vehicle in development by SpaceX. Both of its stages – Super Heavy booster and Starship spacecraft – use liquid oxygen and liquid methane as propellant. Starship’s main features are its very high payload mass capability and low potential operating cost. A tanker variant spacecraft is planned that will refuel other Starships in orbit, increasing the 100 t (220,000 lb) transport range to higher energy orbits and destinations, including the Moon and Mars. The earliest Starship variant will deploy satellites, while later variants will also serve space tourists, or be optimised for lunar landings. Starship’s potentially low cost is key in enabling SpaceX’s Mars ambitions as well as making point-to-point rocket travel on Earth possible.

Starship will launch at Starbase, Kennedy Space Center, and two offshore launch platforms. It would launch upright, with the booster’s thirty-three Raptor engines operating in parallel. After Super Heavy separates, the spacecraft fires its three Raptor Vacuum and three sea-level engines, inserting itself into orbit. The booster then controls its descent via its four grid fins, targeting the launch tower’s arms. At the end of the mission, the Starship spacecraft de-orbits and enters the atmosphere, protected by a series of hexagonal heat shield tiles. The spacecraft then glides towards the landing site using its flaps for control and flips to land.

The rocket was first outlined by SpaceX as early as 2005, with frequent design and name changes as the concept matured. In July 2019, Starhopper, a prototype vehicle with extended fins acting as fixed landing legs, performed a 150 m (490 ft) low altitude test flight under the power of a single Raptor engine. In May 2021, Starship SN15 successfully flew to 10 km (6 mi), transitioning to horizontal free-fall before successfully landing for the first time after four failed attempts by previous prototypes. As of February 2022, the BN4 booster and SN20 spacecraft are scheduled for the first full-stack flight in early 2022, though this schedule is subject to change.

Video credit: SpaceX

Wikipedia dicit:

The Cygnus spacecraft is an expendable American cargo spacecraft developed by Orbital Sciences Corporation and now manufactured and launched by Northrop Grumman Space Systems as part of NASA’s Commercial Resupply Services (CRS) program. It is launched by Northrop Grumman’s Antares rocket or ULA’s Atlas V and is designed to transport supplies to the International Space Station (ISS) following the retirement of the American Space Shuttle.

Since August 2000, ISS resupply missions have been regularly flown by the Russian Progress spacecraft, as well as by the European Automated Transfer Vehicle, and the Japanese H-II Transfer Vehicle. With the Cygnus spacecraft and the SpaceX Dragon, NASA seeks to increase its partnerships with domestic commercial aviation and aeronautics industry.

The Cygnus spacecraft consists of two basic components: the Pressurized Cargo Module (PCM) and the Service Module (SM). The PCM is manufactured by Thales Alenia Space in Turin, (Italy). The initial PCMs have an empty mass of 1,500 kg and a volume of 18 m3·. The service module is built by Orbital ATK and is based on their GEOStar and LEOStar spacecraft buses as well as components from the development of the Dawn spacecraft. It has a gross mass of 1,800 kg with propulsion provided by thrusters using the hypergolic propellants hydrazine and nitrogen tetroxide (the propellant mass is 800 kg). The service module is capable of producing up to 4 kW of electrical power via two gallium arsenide solar arrays. On 12 November 2009, Dutch Space announced it will provide the solar arrays for the initial Cygnus spacecraft.

Video credit: NASA

Wikipedia dicit:

The Aerojet Rocketdyne RS-25, also known as the Space Shuttle Main Engine (SSME), is a liquid-fuel cryogenic rocket engine that was used on NASA’s Space Shuttle. NASA is planning to continue using the RS-25 on the Space Shuttle’s successor, the Space Launch System (SLS).

Designed and manufactured in the United States by Rocketdyne (later known as Pratt & Whitney Rocketdyne and Aerojet Rocketdyne), the RS-25 burns cryogenic liquid hydrogen and liquid oxygen propellants, with each engine producing 1,859 kN (418,000 lbf) of thrust at liftoff. Although the RS-25 can trace its heritage back to the 1960s, the concerted development of the engine began in the 1970s, with the first flight, STS-1, occurring on April 12, 1981. The RS-25 has undergone several upgrades over its operational history to improve the engine’s reliability, safety, and maintenance load.

The engine produces a specific impulse (Isp) of 452 seconds (4.43 km/s) in a vacuum, or 366 seconds (3.59 km/s) at sea level, has a mass of approximately 3.5 tonnes (7,700 pounds), and is capable of throttling between 67% and 109% of its rated power level in one-percent increments. Components of the RS-25 operate at temperatures ranging from −253 to 3,300 °C (−400 to 6,000 °F).

The Space Shuttle used a cluster of three RS-25 engines mounted in the stern structure of the orbiter, with fuel being drawn from the external tank. The engines were used for propulsion during the entirety of the spacecraft’s ascent, with additional thrust being provided by two solid rocket boosters and the orbiter’s two AJ10 orbital maneuvering system engines. Following each flight, the RS-25 engines were removed from the orbiter, inspected, and refurbished before being reused on another mission. On Space Launch System flights, the engines will be expendable. For the first four flights, engines left over from the Space Shuttle program will be refurbished and used before NASA switches to the simplified RS-25E variant.

Video credit: NASA’s Kennedy Space Center