OrbitalHub

Wikipedia dicit:

Omega, stylized as “OmegA”, is a launch vehicle in development by Northrop Grumman as an NSSL replacement program intended for national security and commercial satellites.

Omega is similar to the defunct Ares I and Liberty projects, both of which consisted of a five segment Space Shuttle Solid Rocket Booster (SRB) and a cryogenic second stage. Ares I would have combined a five-segment SRB with a J-2X powered second stage, while Liberty would have used a five-segment SRB with the core stage of the European Ariane 5 as a second stage. By comparison, Omega consists of Space Shuttle-derived solid stages with a cryogenic upper stage provided by Aerojet Rocketdyne (replacing earlier plans to use an upper stage provided by Blue Origin). It is intended to be launched from Kennedy Space Center LC-39B or Vandenberg Air Force Base SLC-2.

Omega is proposed as a vehicle to launch national security satellites for the United States Air Force, and could launch other government and commercial payloads, including to geostationary transfer orbit. Crewed spacecraft could also be launched, just as the predecessor Ares I and Liberty rockets, which were designed to launch the Orion space capsule.

Video Credit: Northrop Grumman

Wikipedia dicit:

The Proton-M launch vehicle consists of three stages; all of them powered by liquid rocket engines using the hypergolic propellant combination of dinitrogen tetroxide as the oxidizer, and unsymmetrical dimethylhydrazine for fuel.

The first stage is unique in that it consists of a central cylindrical oxidizer tank with the same diameter as the other two stages with six fuel tanks attached to its circumference, each carrying an engine. The engines in this stage can swivel tangentially up to 7° from the neutral position, providing full thrust vector control. The rationale for this design is logistics: the diameter of the oxidizer tanks and the two following stages is the maximum that can be delivered by railroad to Baikonur. However, within Baikonur the fully assembled stack is transported again by rail, as it has enough clearance.

The second stage uses a conventional cylindrical design. It is powered by three RD-0210 engines and one RD-0211 engine. The RD-0211 is a modified version of the RD-0210 used to pressurize the propellant tanks. The second stage is joined to the first stage through a net instead of a closed inter-stage, to allow the exhaust to escape because the second stage begins firing seconds before separation. Thrust vector control is provided by engine gimballing.

The third stage is also of a conventional cylindrical design. It contains the avionics system that controls the first two stages. It uses one RD-0213 which is a fixed (non-gimballed) version of the RD-0210, and one RD-0214 which is a four nozzle vernier engine used for thrust vector control. The nozzles of the RD-0214 can turn up to 45°; they are placed around (with some separation), and moderately above the nozzle of the RD-0213.

The Proton-M features modifications to the lower stages to reduce structural mass, increase thrust, and utilise more propellant (less of it remains unused in the tanks). A closed-loop guidance system is used on the first stage, which allows more complete consumption of propellant. This increases the rocket’s performance slightly compared to previous variants, and reduces the amount of toxic chemicals remaining in the stage when it impacts downrange. It can place up to 21 tonnes (46,000 lb) into low Earth orbit. With an upper stage, it can place a 3 tonne payload into geosynchronous orbit, or a 5.5 tonne payload into geosynchronous transfer orbit. Efforts were also made to reduce dependency on foreign component suppliers.

Video Credit: Roscosmos

Wikipedia dicit:

Yamal 601 (Russian: Ямал-601) is a geostationary communications satellite ordered by Gazprom Space Systems to ISS Reshetnev on the Ekspress-2000 platform for its Yamal program. The Ekspress-2000 platform is the heavy version, which can weigh up to 3,500 kg (7,700 lb) and generate up to 14 kW of power on an unpressurized bus designed for direct GEO injection with 15 years of design life. Its payload will be supplied by Thales Alenia Space and is composed of 38 C band, and 32 Ka band transponders. It will replace Yamal 202 on 49°E when it reaches its end of service around 2018.

Video Credit: Roscosmos

NASA dicit:

NASA’s Orion, Space Launch System (SLS), and Exploration Ground Systems (EGS) programs are continuing work on one of the most complex and sophisticated space systems ever built. Across America and in Europe, teams are developing and building the spacecraft, rocket, and infrastructure necessary to send humans to deep space destinations including the surface of the Moon and beyond.

Some major recent milestones include: Orion – Crew Module Uprighting System Test at Atlantic Beach, North Carolina; European Service Module Solar Array Expanded; Fit Check in the Super Guppy Aircraft; Ascent Abort-2 Launch Abort System Stacking and Integration at Kennedy Space Center in Cape Canaveral, Florida; Launch Abort System Attitude Control Motor Test in Elkton, Maryland. SLS – Liquid Oxygen Tank and Forward Skirt join at Michoud Assembly Facility in New Orleans, Liquid Hydrogen Tank Structural Test Article Unload from Pegasus Barge at Marshall Space Flight Center in Huntsville, Alabama; RS-25 Engine Testing at Stennis Space Center in Bay St. Louis, Mississippi; Core Stage-1 Engine Section and Boat Tail Completed and Mated at Michoud. EGS – at NASA’s Kennedy Space Center: Core Stage Intertank Umbilical Swing Testing; Launch Pad 39B Upgrades; Crawler Engine Maintenance.

Video Credit: NASA Johnson

Wikipedia dicit:

The Vulcan rocket is an American heavy-payload launch vehicle under development since 2014 by United Launch Alliance (ULA), funded by a public–private partnership with the U.S. government. ULA expects the first launch of the new rocket to occur in April 2021.

United Launch Alliance had considered several launch vehicle concepts in the decade since the company was formed in 2006. Various concepts for derivative vehicles based on the Atlas and Delta lines of launch vehicles they inherited from their predecessor companies were presented to the U.S. government for funding. None were funded beyond concept stage.

In early 2014, geopolitical and U.S. political considerations involving international sanctions during the Ukrainian crisis, led to an effort by ULA to consider possibly replacing the Russian-supplied RD-180 engine used on the first stage booster of the Atlas V. Formal study contracts were issued by ULA in June 2014 to several U.S. rocket engine suppliers. ULA was also facing competition from SpaceX, then seen to affect ULA’s core national security market of U.S. military launches, and by July 2014 the United States Congress was debating whether to legislate a ban on future use of the RD-180.

In September 2014, ULA announced that it had entered into a partnership with Blue Origin to develop the BE-4 liquid oxygen (LOX) and liquid methane (CH4) engine to replace the RD-180 on a new first stage booster. The Blue engine was already in its third year of development by Blue Origin, and ULA said it expected the new stage and engine to start flying no earlier than 2019. Two of the 2,400-kilonewton (550,000 lbf)-thrust BE-4 engines were to be used on a new launch vehicle booster. ULA referred to the successor concept vehicle as a “next generation launch system” and used that descriptor into early 2015.

In October 2014, ULA announced a major restructuring of company processes and workforce to reduce launch costs by half. One of the reasons given for the restructuring and new cost reduction goals was new competition in the launch market from SpaceX. ULA planned to have preliminary design ideas in place for a blending of its existing Atlas V and Delta IV technologies by the end of 2014, to build a successor to the Atlas V that would allow the company to halve Atlas V launch costs. A part of the restructuring effort was described as the effort to co-develop the alternative BE-4 engine with Blue Origin for the new launch vehicle.

Video Credit: ULA

Blue Origin dicit:

New Shepard had a great mission on May 2, 2019. This particular rocket has flown to space and back 5 times. The mission flew 38 payloads for a variety of schools, universities, government agencies and private companies.

Video Credit: Blue Origin