OrbitalHub

Wikipedia dicit:

New Shepard is a vertical-takeoff, vertical-landing (VTVL), crew-rated suborbital launch vehicle developed by Blue Origin as a commercial system for suborbital space tourism.
The name New Shepard makes reference to the first American astronaut in space, Alan Shepard, one of the original NASA Mercury Seven astronauts, who ascended to space in 1961 on a suborbital trajectory similar to that of New Shepard.

Prototype engine and vehicle flights began in 2006, while full-scale engine development started in the early 2010s and was complete by 2015. Uncrewed flight testing of the complete New Shepard vehicle (propulsion module and space capsule) began in 2015.

On 23 November 2015, after reaching 100.5 km (62.4 mi) altitude (outer space), the suborbital New Shepard booster successfully performed a powered vertical soft landing, the first time a suborbital booster rocket had returned from space to make a successful vertical landing. The test program continued in 2016 and 2017 with four additional test flights made with the same vehicle (NS-2) in 2016 and the first test flight of the new NS-3 vehicle made in 2017.

Blue Origin planned its first crewed test flight to occur in 2019, which was however delayed until 2021, and has since announced that tickets would begin to be sold for commercial flights of up to six people. The first crewed flight took place on 20 July 2021. An anonymous buyer purchased one seat for the 20 July 2021 flight at auction for $28 million but this person did not fly on said flight due to scheduling problems; the anonymous buyer was rescheduled for a later flight. Instead of the auction winning passenger, 18-year-old Oliver Daemen was selected to fly. Daemen’s father paid for his flight, thus Daemen was the first customer (i.e. person whose flight has been paid for) passenger of New Shepard, and became the youngest person and first teenager to fly into space. As of October 13th, 2021, New Shepard has flown 8 passengers into space.

Video credit: Blue Origin

NASA dicit:

SpaceX CRS-23, also known as SpX-23, is a Commercial Resupply Service mission to the International Space Station. The mission was contracted by NASA and was flown by SpaceX using the Cargo Dragon C208. This was the third flight for SpaceX under NASA’s CRS Phase 2 contract awarded in January 2016. A NASA Flight Planning Integration Panel (FPIP) from 2019 indicates that SpaceX cargo missions will begin to extend their duration to 60 days and beyond starting with CRS-23.

SpaceX plans to reuse the Cargo Dragons up to five times. The Cargo Dragon launches without SuperDraco abort engines, without seats, cockpit controls and the life support system required to sustain astronauts in space. This newer design provides several benefits, including a faster process to recover, refurbish and re-fly versus the earlier Dragon CRS design used for ISS cargo missions.

The GITAI S1 Robotic Arm Tech Demo will test GITAI Japan Inc.’s microgravity robot by placing the arm inside the newly added Nanoracks Bishop Airlock, which was carried to the station by Dragon C208.2 during the SpaceX CRS-21 mission last year. Once inside the airlock, the arm will perform numerous tests to demonstrate its versatility and dexterity.

Designed by GITAI Japan Inc., the robot will work as a general-purpose helper under the pressurized environment inside the Bishop Airlock. It will operate tools and switches and run scientific experiments. The next step will be to test it outside the ISS in the harsh space environment. The robot will be able to perform tasks both autonomously and via teleoperations. Its arm has eight degrees of freedom and a 1-meter reach. GITAI S1 is a semi-autonomous/semi-teleoperated robotic arm designed to conduct specified tasks internally and externally on space stations, on-orbit servicing, and lunar base development. By combining autonomous control via AI and teleoperations via the specially designed GITAI manipulation system H1, GITAI S1 on its own, possesses the capability to conduct generous-purpose tasks (manipulation of switches, tools, soft objects; conducting science experiments and assembly; high-load operations; etc.) that were extremely difficult for industrial robots such as task specific robotic arms to do.

Video credit: NASA/SpaceX

SpaceX dicit:

On Wednesday, May 5, Starship serial number 15 (SN15) successfully completed SpaceX’s fifth high-altitude flight test of a Starship prototype from Starbase in Texas. SN15 ascended, transitioned propellant, and reoriented itself for reentry and a controlled aerodynamic descent. The Raptor engines reignited to perform the landing flip maneuver before touching down for a nominal landing on the pad.

These Starship test flights improve our understanding and development of a fully reusable transportation system designed to carry crew and cargo on long-duration interplanetary flights, help humanity return to the Moon, and travel to Mars and beyond.

Video credit: SpaceX

SpaceX dicit:

The SpaceX team attempted a high-altitude flight test of Starship serial number 15 (SN15) – our fifth high-altitude flight test of a Starship prototype from Starbase in Texas. SN15 has vehicle improvements across structures, avionics and software, and the engines that will allow more speed and efficiency throughout production and flight: specifically, a new enhanced avionics suite, updated propellant architecture in the aft skirt, and a new Raptor engine design and configuration.

Similar to previous high-altitude flight tests of Starship, SN15 is powered through ascent by three Raptor engines, each shutting down in sequence prior to the vehicle reaching apogee – approximately 10 km in altitude. SN15 performed a propellant transition to the internal header tanks, which hold landing propellant, before reorienting itself for reentry and a controlled aerodynamic descent.

The Starship prototype descended under active aerodynamic control, accomplished by independent movement of two forward and two aft flaps on the vehicle. All four flaps are actuated by an onboard flight computer to control Starship’s attitude during flight and enable precise landing at the intended location. SN15’s Raptor engines then reignited as the vehicle attempted a landing flip maneuver immediately before touching down on the landing pad adjacent to the launch mount.

A controlled aerodynamic descent with body flaps and vertical landing capability, combined with in-space refilling, are critical to landing Starship at destinations across the solar system where prepared surfaces or runways do not exist, and returning to Earth. This capability will enable a fully reusable transportation system designed to carry both crew and cargo on long-duration, interplanetary flights and help humanity return to the Moon, and travel to Mars and beyond.

Video credit: SpaceX

SpaceX dicit:

The SpaceX team attempted a high-altitude flight test of Starship serial number 11 (SN11) – our fourth high-altitude flight test of a Starship prototype from Starbase in Texas. Similar to previous high-altitude flight tests of Starship, SN11 was powered through ascent by three Raptor engines, each shutting down in sequence prior to the vehicle reaching apogee – approximately 10 km in altitude. SN11 performed a propellant transition to the internal header tanks, which hold landing propellant, before reorienting itself for reentry and a controlled aerodynamic descent.

A controlled aerodynamic descent with body flaps and vertical landing capability, combined with in-space refilling, are critical to landing Starship at destinations across the solar system where prepared surfaces or runways do not exist, and returning to Earth. This capability will enable a fully reusable transportation system designed to carry both crew and cargo on long-duration, interplanetary flights and help humanity return to the Moon, and travel to Mars and beyond.

Video credit: SpaceX

NASA dicit:

Video shows engineers at NASA’s Marshall Space Flight Center in Huntsville, Alabama, completing the welds to form the launch vehicle stage adapter (LVSA) for NASA’s Space Launch System (SLS) rocket. The launch vehicle stage adapter in this video will fly on Artemis II, the first crewed mission of NASA’s Artemis program. Upon stacking the upper and lower cones, technicians use advanced robotic tooling and an innovative process called friction stir welding, to join the cones of the LVSA to form one structure.

The next step in the manufacturing process is the installation of the pneumatically actuated frangible joint which sits atop the LVSA and helps separate the core stage and LVSA from the Interim Cryogenic Propulsion Stage (ICPS) during flight. After the core stage launches the rocket, the ICPS provides the power to send the Orion spacecraft and its crew to the Moon.

Video credit: NASA’s Marshall Space Flight Center