OrbitalHub

Wikipedia dixit:

“The Interplanetary Transport System (ITS), formerly known as the Mars Colonial Transporter (MCT), is SpaceX’s privately funded development project to design and build a spaceflight system of reusable rocket engines, launch vehicles and spacecraft to transport humans to Mars and return to Earth. SpaceX began development of the large Raptor rocket engine for the Mars Colonial Transporter before 2014. As of June 2016, publicly-announced company conceptual plans included the first Mars-bound cargo flight of ITS launching no earlier than 2022, followed by the first ITS Mars flight with passengers one synodic period later in 2024, following two preparatory research launches of Mars probes in 2018 and 2020 on Dragon/Falcon Heavy equipment. SpaceX CEO Elon Musk unveiled details of the space mission architecture at the 67th International Astronautical Congress on 27 September 2016. The booster will have a diameter of 12 m, the spaceship diameter will be 17 m and stack height of the entire vehicle will be 122 m. The selected fuel type is deep-cryo methalox for 42 Raptor engines on the booster and 9 on the spacecraft.

As early as 2007, Elon Musk stated a personal goal of eventually enabling human exploration and settlement of Mars. Bits of additional information about the mission architecture were released in 2011–2015, including a 2014 statement that initial colonists would arrive at Mars no earlier than the middle of the 2020s. Company plans as of mid-2016 continue to call for the arrival of the first humans on Mars no earlier than 2025.

Musk stated in a 2011 interview that he hoped to send humans to Mars’ surface within 10–20 years, and in late 2012 he stated that he envisioned a Mars colony of tens of thousands with the first colonists arriving no earlier than the middle of the 2020s. In October 2012, Musk articulated a high-level plan to build a second reusable rocket system with capabilities substantially beyond the Falcon 9/Falcon Heavy launch vehicles on which SpaceX had by then spent several billion US dollars. This new vehicle was to be “an evolution of SpaceX’s Falcon 9 booster… much bigger [than Falcon 9].” But Musk indicated that SpaceX would not be speaking publicly about it until 2013. In June 2013, Musk stated that he intended to hold off any potential IPO of SpaceX shares on the stock market until after the “Mars Colonial Transporter is flying regularly.”

In February 2014, Musk stated that Mars Colonial Transporter will be “100 times the size of an SUV”, and capable of taking 100 tons of cargo to Mars. Also, SpaceX engine development head Tom Mueller said SpaceX would use nine Raptor engines on a single rocket, similar to the use of nine Merlin engines on each Falcon 9 booster core. He said “It’s going to put over 100 tons of cargo on Mars.” In early 2014, it appeared that the large rocket core that would be used for the booster to be used with MCT would be at least 10 meters (33 ft) in diameter, nearly three times the diameter and over seven times the cross-sectional area of the Falcon 9 booster cores. In August 2014, media sources speculated that the initial flight test of the Raptor-driven super-heavy launch vehicle could occur as early as 2020, in order to fully test the engines under orbital spaceflight conditions; however, any colonization effort was reported to continue to be “deep into the future”.

In January 2015, Musk said that he hoped to release details of the “completely new architecture” for the Mars transport system in late 2015 but those plans changed and, by December 2015, the plan to publicly release additional specifics had moved to 2016. In January 2016, Musk indicated that he hoped to describe the architecture for the Mars missions with the next generation SpaceX rocket and spacecraft later in 2016, at the 67th International Astronautical Congress conference, in September 2016. Musk stated in June 2016 that the first unmanned MCT Mars flight was planned for departure in 2022, to be followed by the first manned MCT Mars flight departing in 2024. By September 2016, Musk noted that the MCT name would not continue, as the system would be able to “go well beyond Mars”, and that a new name would be needed: Interplanetary Transport System (ITS), with the first spacecraft named “Heart of Gold” in reference to the Infinite Improbability Drive.”

Video credit: SpaceX

NASA dixit:

“On Sept. 8, NASA launched the Origins Spectral Interpretation Resource Identification Security – Regolith Explorer, or OSIRIS-REx mission from Cape Canaveral Air Force Station in Florida. OSIRIS-REx is the first U.S. mission to sample an asteroid. The spacecraft is scheduled to arrive at near-Earth asteroid Bennu in 2018, survey the asteroid’s surface, retrieve at least 60 grams (2.1 ounces) of surface material, and return the sample to Earth in 2023 for study. Analysis of the sample will reveal the earliest stages of the solar system’s evolution and the history of Bennu over the past 4.5 billion years.”

Video credit: NASA/ULA

NASA dixit:

“On Sept. 6, after bidding farewell to the crew remaining aboard the International Space Station, Expedition 48 Commander Jeff Williams of NASA and Soyuz Commander Alexey Ovchinin and Flight Engineer Oleg Skripochka of Roscosmos undocked from the orbital outpost to begin their return trip to Earth. They spent 172 days aboard the ISS, conducting research and operational work in support of the station.”

Video credit: NASA

NASA dixit:

“The SpaceX CRS-9 Dragon cargo craft departed the International Space Station Aug. 26 after five weeks at the complex. Dragon delivered critical science experiments and the first International Docking Adapter to which U.S. commercial spacecraft will link up to in the future. Using the Canadarm2 robotic arm, Expedition 48 Commander Jeff Williams and Flight Engineer Kate Rubins released the Dragon and monitored the resupply spacecraft as it backed away to a safe distance from the station for its deorbit engine firing that would enable the ship to enter the Earth’s atmosphere for a parachute-assisted splashdown in the Pacific Ocean west of Baja California. Dragon returned about one and a half tons of science experiments and other cargo that will be collected once it reaches port in Long Beach, California. Dragon launched July 18 atop a SpaceX Falcon 9 rocket from Cape Canaveral Air Force Station in Florida and arrived at the station July 20.”

Video credit: NASA

United Launch Alliance dixit:

“The Air Force’s AFSPC-6 payload, encapsulated inside a 4-meter diameter payload fairing, is transported and mated to a Delta IV rocket at Space Launch Complex-37. AFSPC-6 will deliver two Geosynchronous Space Situational Awareness Program (GSSAP) satellites to near-geo­synchronous orbit. The twin GSSAP spacecraft, built by Orbital ATK, will support U.S. Strategic Command space enhanced awareness operations.”

Wikipedia dixit:

“Air Force Space Command (AFSPC) is a major command of the United States Air Force, with its headquarters at Peterson Air Force Base, Colorado. AFSPC supports U.S. military operations worldwide through the use of many different types of satellite, launch and cyber operations. Operationally, AFSPC is an Air Force component command subordinate to U.S. Strategic Command (USSTRATCOM), a unified combatant command.

More than 38,000 people perform AFSPC missions at 88 locations worldwide and comprises Regular Air Force, Air Force Reserve and Air National Guard military personnel, Department of the Air Force Civilians (DAFC), and civilian military contractors. Composition consist of approximately 22,000 military personnel and 9,000 civilian employees, although their missions overlap.

AFSPC gained the cyber operations mission with the stand-up of 24th Air Force under AFSPC in August 2009. On 1 December 2009, the strategic nuclear intercontinental ballistic missile (ICBM) mission that AFSPC inherited from Air Combat Command (ACC) in 1993, and which ACC had inherited following the inactivation of Strategic Air Command (SAC) in 1992, was transferred to the newly established Air Force Global Strike Command (AFGSC). Spacelift operations at the East and West Coast launch bases provide services, facilities and range safety control for the conduct of DOD, NASA and commercial launches. Through the command and control of all DOD satellites, satellite operators provide force-multiplying effects—continuous global coverage, low vulnerability and autonomous operations. Satellites provide essential in-theater secure communications, weather and navigational data for ground, air and fleet operations and threat warning. Ground-based radar and Defense Support Program satellites monitor ballistic missile launches around the world to guard against a surprise missile attack on North America. Space surveillance radars provide vital information on the location of satellites and space debris for the nation and the world.

As of 2013, Air Force Space Command is considering Space Disaggregation, which would involve replacing a few large multimission satellites with larger numbers of smaller single purpose platforms. This could be used to defend against ASATs, by increasing the number of targets that needed to be attacked.”

Video credit: United Launch Alliance

Ergo dixit:

The NRO satellites are operated by the United States National Reconnaissance Office. The NRO missions are generally classified, so their exact purposes and orbital elements are not available to the public.

Wikipedia dixit:

“The Atlas V was developed by Lockheed Martin Commercial Launch Services as part of the US Air Force Evolved Expendable Launch Vehicle (EELV) program and made its inaugural flight on August 21, 2002. The vehicle operates out of Space Launch Complex 41 at Cape Canaveral Air Force Station and Space Launch Complex 3-E at Vandenberg Air Force Base. Lockheed Martin Commercial Launch Services continues to market the Atlas V to commercial customers worldwide.

The Atlas V first stage, the Common Core Booster (CCB), is 12.5 ft (3.8 m) in diameter and 106.6 ft (32.5 m) in length. It is powered by a single Russian RD-180 main engine burning 627,105 lb (284,450 kg) of liquid oxygen and RP-1. The booster operates for about four minutes, providing about 4 meganewtons (860,000 lbf) of thrust. Thrust can be augmented with up to five Aerojet strap-on solid rocket boosters, each providing an additional 1.27 meganewtons (285,500 lbf) of thrust for 94 seconds. The Atlas V is the newest member of the Atlas family. Compared to the Atlas III vehicle, there are numerous changes. Compared to the Atlas II, the first stage is a near-redesign. There was no Atlas IV. The “1.5 staging” technique was dropped on the Atlas III, although the same RD-180 engine is used. The RD-180 features a dual-combustion chamber, dual-nozzle design and is fueled by a kerosene/liquid oxygen mixture. The main-stage diameter increased from 10 feet to 12.5 feet. As with the Atlas III, the different mixture ratio of the engine called for a larger oxygen tank (relative to the fuel tank) compared to Western engines and stages. The first stage tanks no longer use stainless steel monocoque “balloon” construction. The tanks are isogrid aluminum and are structurally stable when unpressurized. Use of aluminum, with a higher thermal conductivity than stainless steel, requires insulation for the liquid oxygen. The tanks are covered in a polyurethane-based layer. Accommodation points for parallel stages, both smaller solids and identical liquids, are built into first stage structures.

The Centaur upper stage uses a pressure stabilized propellant tank design and cryogenic propellants. The Centaur stage for Atlas V is stretched 5.5 ft (1.68 m) relative to the Atlas IIAS Centaur and is powered by either one or two Aerojet Rocketdyne RL10A-4-2 engines, each engine developing a thrust of 99.2 kN (22,300 lbf). The inertial navigation unit (INU) located on the Centaur provides guidance and navigation for both the Atlas and Centaur, and controls both Atlas and Centaur tank pressures and propellant use. The Centaur engines are capable of multiple in-space starts, making possible insertion into low Earth parking orbit, followed by a coast period and then insertion into GTO. A subsequent third burn following a multi-hour coast can permit direct injection of payloads into geostationary orbit. As of 2006, the Centaur vehicle had the highest proportion of burnable propellant relative to total mass of any modern hydrogen upper stage and hence can deliver substantial payloads to a high energy state.

The standard payload fairing sizes are 4 or 5 meters in diameter. The 4.2-meter fairing, originally designed for the Atlas II booster, comes in three different lengths, the original 9-meter high version, as well as fairings 10 meters (first flown on the AV-008/Astra 1KR launch) and 11 meters (seen on the AV-004/Inmarsat-4 F1 launch) high. Lockheed Martin had the 5.4-meter (4.57 meters usable) payload fairing for the Atlas V developed and built by RUAG Space (former Oerlikon Space) in Switzerland. The RUAG fairing uses carbon fiber composite construction, based on flight-proven hardware from the Ariane 5. Three configurations will be manufactured to support the Atlas V. The short (10-meter long) and medium (13-meter long) configurations will be used on the Atlas V 500 series. The 16-meter long configuration would be used on the Atlas V Heavy. The classic fairing covers only the payload, leaving the Centaur stage exposed to open air. The RUAG fairing encloses the Centaur stage as well as the payload.”

Video credit: United Launch Alliance