OrbitalHub

Credits: NASA

Orbital will employ its Taurus II medium-lift launch vehicle and the Cygnus spacecraft in order to service the International Space Station (ISS) under the Commercial Resupply Services (CRS) contract.

Orbital is one of the two companies awarded CRS contracts under the Commercial Orbital Transportation Services Project (COTS).

NASA announced the COTS project on January 18, 2006. The purpose of the program is to stimulate the development of access to low Earth orbit (LEO) in the private sector. At the time, with the imminent retirement of the Space Shuttle fleet, NASA was faced with the option of buying orbital transportation services on foreign launch systems: the Russian Soyuz / Progress, the European Ariane 5 / ATV, or the Japanese H-II / HTV.

Another factor taken into consideration by NASA was that competition in the free market could lead to the development of more efficient and affordable launch systems compared to launch systems that a government agency could build and operate.

Credits: Orbital

Orbital relies on proven experience in launch vehicle technology. Taurus II is designed to provide low-cost and reliable access to space, and it uses systems from other members of Orbital’s family of successful launchers: Pegasus, Taurus, and Minotaur.

Taurus II is a two-stage launch vehicle that can use an additional third stage for achieving higher orbits. The payloads handled by Taurus II can have a mass of up to 5,400 kg.

Orbital is responsible for overall development and integration of the first stage. The two AJ26-62, designed and produced by Aerojet and Orbital, are powered by liquid oxygen and kerosene. The core design is driven by NPO Yuzhnoye, the designer of the Zenit launchers.

The AJ26-62 engines are basically the NK-33 engines designed by the Kuznetsov Design Bureau for the Russian N-1 launch vehicle, and remarketed by Aerojet under a new designation.

The second stage uses an ATK Castor-30 solid motor with thrust vectoring. This stage evolved from the Castor-120 solid stage.

The optional third stage is developed by Orbital. The stage was dubbed the Orbit Raising Kit (ORK) and it uses a helium pressure regulated bi-propellant propulsion system powered by nitrogen tetroxide and hydrazine. ORK evolved from the Orbital STAR Bus. Because it is a hypergolic stage, it allows several burns to be performed in orbit, and can be used for high-precision injections using various orbital profiles.

Credits: Orbital

Cygnus will only have cargo capability and will be able to deliver up to 2,300 kg of pressurized or un-pressurized cargo to the ISS. The spacecraft will also be able to return up to 1,200 kg of cargo from ISS to Earth.

The two components of the Cygnus spacecraft will be the service module and the cargo module.

The service module is based on the Orbital STAR bus (like the ORK stage), and will use two solar arrays for producing electrical power for the navigation systems onboard.

The pressurized cargo module is based on the Italian-built Multi-Purpose Logistics Module (MPLM). The un-pressurized cargo module is based on NASA’s ExPRESS Logistics Carrier.

Cygnus will not dock to the ISS in the same manner as the European ATV, but it will be able to maneuver close to the ISS where the Canadarm 2 robotic arm will be used to capture it and berth it to the Node 2 module, similar to the Japanese HTV or SpaceX’s Dragon spacecraft.

The Mid-Atlantic Regional Spaceport (MARS), located at NASA’s Wallops Island Flight Facility on Virginia’s Eastern shore, was chosen by Orbital to serve as the base of operations for the Taurus II launch vehicle.

MARS has two FAA licensed launch pads for LEO access. MARS also offers access to suborbital launchers, vehicle and payload storage, and processing and launch facilities.

Credits: NASA

Due to the location of the spaceport, latitude 37.8 degrees N, longitude 75.5 degrees W, optimal orbital inclinations for the launches performed at MARS are between 38 and 60 degrees. Polar and retrograde orbits can also be serviced with additional in-flight maneuvering.

The first flight of Orbital’s new Taurus II / Cygnus launch system under COTS is scheduled for late 2010.

The awarded contracts are fixed-price indefinite delivery, indefinite quantity contracts. They will begin January 1, 2009, and are effective through December 31, 2016. SpaceX and Orbital each will have to deliver a minimum of twenty metric tons of cargo to the space station, and they will also have to deliver non-standard services in support of the cargo resupply, including analysis and special tasks as the government deems necessary.

SpaceX will service the ISS with its Falcon9/Dragon system.

“The SpaceX team is honored to have been selected by NASA as the winner of the Cargo Resupply Services contract,” said Elon Musk, CEO and CTO, SpaceX. “This is a tremendous responsibility, given the swiftly approaching retirement of the Space Shuttle and the significant future needs of the Space Station. This also demonstrates the success of the NASA COTS program, which has opened a new era for NASA in US Commercial spaceflight.”

Orbital will employ the Taurus II^TM medium-lift launch vehicle and the Cygnus^TM maneuvering space vehicle.

“We are very appreciative of the trust NASA has placed with us to provide commercial cargo transportation services to and from the International Space Station, beginning with our demonstration flight scheduled in late 2010,” said Mr. David W. Thompson, Orbital’s Chairman and Chief Executive Officer. “The CRS program will serve as a showcase for the types of commercial services U.S. space companies can offer NASA, allowing the space agency to devote a greater proportion of its resources for the challenges of human spaceflight, deep space exploration and scientific investigations of our planet and the universe in which we live.”

Both Orbital and SpaceX have issued press releases with more details about the CRS contracts.

Credits: SpaceX

Another critical milestone has been reached by SpaceX with the arrival of Falcon 9 hardware at Cape Canaveral.

After the full mission-length firing test of the Falcon 9 first stage engines and the firing test of the Dragon maneuvering thruster, the arrival of the Falcon 9 first stage fuel tank fulfills SpaceX’s commitment to having Falcon 9 hardware at Cape Canaveral by year-end.

“Christmas has arrived a few days early for our team at the Cape,” said Brian Mosdell, Director of Florida Launch Operations for SpaceX. “The packages measure extra large this year, and they will keep everyone busy in the coming weeks.”

All of the Falcon 9 elements and the ground support hardware have already left the SpaceX manufacturing facility in Hawthorne, California. The hardware will make its way to the launch site at Cape Canaveral over the next two weeks. The Falcon 9 will then be assembled on horizontal and raised to vertical on the custom built erector.

Credits: SpaceX

There are four Falcon 9 launches scheduled for 2009. Two of these launches are demonstration flights with the Dragon spacecraft as part of the NASA Commercial Orbital Transportation Services (COTS) competition. A total of three flights of the Falcon 9/Dragon launch system will be conducted under the agreement, in order to demonstrate cargo delivery capability to the International Space Station (ISS).

NASA’s agreement with SpaceX can be extended to include demonstrating transport of crew to and from the ISS.

“2008 has been a year of rapid progress for SpaceX,” said Elon Musk, CEO and CTO of SpaceX. “The delivery of the Falcon 9 to the Cape is a major milestone in designing and deploying the most reliable, cost-efficient fleet of launch vehicles in the world. I applaud our SpaceX team who has worked 24/7 to make this happen.”

SpaceX has made available a video of Elon Musk giving a tour of the SpaceX Falcon 9 launch site at Space Launch Complex 40, Cape Canaveral AFS, Florida.

Credits: XCOR Aerospace

XCOR completed the first test fire of the rocket engine that will power the Lynx suborbital launch vehicle. The test was performed on Monday, December 15, 2008, at XCOR’s rocket test facility located at the Mojave Air and Space Port.

The rocket engine is designated as 5K18. The engine is powered by liquid oxygen and kerosene and can produce up to 2900 lbf of thrust.

The 5K18 is the eleventh in a series of rocket engines that XCOR has designed and fired during its nine years of existence.

“Today’s successful hot fire marks an important step forward in building the Lynx,” said XCOR CEO Jeff Greason. “The 5K18 builds on our previous experience in designing and building reliable, durable and fully reusable rocket engines from 15 lbf thrust up to 7500 lbf, that will make it possible to provide affordable access to space.”

The Lynx will use four 5K18 engines and it will be able to perform suborbital flights. Space tourists can buy tickets to fly on the Lynx for $95,000 through RocketShip Tours. The full press release is available on the XCOR Aerospace web site.

Credits: NASA

Last week we presented GOSAT a.k.a. Ibuki, a mission that has as its objective the mapping of carbon dioxide and methane in the Earth’s atmosphere. A similar mission is getting ready to launch on the other side of the Pacific: the Orbiting Carbon Observatory (OCO). OCO is a NASA Earth System Science Pathfinder (ESSP) Program mission.

The mission team includes the Orbital Sciences Corporation, the Jet Propulsion Laboratory, and Hamilton Sundstrand Sensor Systems.

The atmospheric carbon dioxide (CO₂) is an important greenhouse gas. CO₂ absorbs and traps infrared radiation emitted by the Earth’s surface, preventing it from escaping to space. OCO will provide global CO₂ measurements from space. The data collected during the mission will help scientists understand the global carbon cycle. This understanding is essential to improve the predictions of future atmospheric CO₂ increases and its impact on the climate.

The OCO has a mass of 407 kg. The two GaAs solar arrays will provide 324 W orbit average for the scientific payload onboard. The satellite will use hydrazine thrusters for stabilization while on orbit. The estimated life span for the mission is 24 months.

The scientific payload includes three spectrometers. The spectrometers can detect what gases are in the Earth’s atmosphere and determine their amounts. The measurements will translate into monthly estimates of atmospheric CO₂ over 621-square-mile regions of the Earth’s surface. From its sun-synchronous orbit, OCO will map the globe once every sixteen days. These maps will help locate CO₂ sources and sinks.

Credits: NASA / Orbital

OCO will be placed on orbit by a Taurus XL launch vehicle. Taurus XL is a solid fuel launch vehicle built by the Orbital Sciences Corporation. According to the Taurus fact sheet, it provides launch capability for satellites weighing up to 1,590 kg. The range of launch missions supported by Taurus include low inclination low Earth orbit (LEO), polar LEO, sun-synchronous LEO, geo-transfer orbit, and interplanetary trajectory.

Depending on the configuration, Taurus can have a mass from 69,000 to 77,000 kg and can have a length from 27 to 32 m.

The mission launch is scheduled for early 2009. The Taurus XL launch vehicle will lift off from Vandenberg Air Force Base, California.

Credits: NASA

One of the crucial requirements for a man-rated launch system is a reliable Launch Abort System (LAS). LAS is basically a top-mounted rocket connected to a crew module and it is used to separate the crew module from the rest of the launch vehicle in case of emergency.

An emergency can be anything from an explosion of the launch vehicle on the launch pad to a failed separation of the lower stage during flight.

In the case of the Orion Module, several designs were considered for the LAS: the Multiple External Service Module Abort Motor concept, the Crew Module Strap On Motors concept, and the In-Line Tandem Tractor (Tower) concept. The latter concept was incorporated in the Ares I/Orion design.

The Tandem Tractor (Tower) design of the LAS has three motors: an Attitude Control Motor (eight nozzles), a Jettison Motor (four aft nozzles), and the Abort Motor (four exposed flow nozzles). These motors will make possible the separation of the module and the control of the flight after the separation from the launch vehicle. An important component of the LAS is the Boost Protective Cover (BPC), which protects the crew module from the exhaust of the motors.

Credits: NASA

The LAS is designed to perform on the launch pad as well as during the first 300,000 feet after the launch. There are three possible scenarios for the abort procedure: on the launch pad, on the mid-altitude flight segment (up to an altitude of 150,000 feet), and on the high-altitude flight segment (from 150,000 feet to 300,000 feet, where the LAS is jettisoned on a nominal flight). Tests will have to be performed to cover these scenarios: on the launch pad as well in flight.

NASA has made available animations of the test flights planned for the LAS. One is the animation of the Orion Module LAS pad abort flight test. The second presents the Orion Module LAS ascent abort flight test.

Credits: NASA

Currently, the Launch Abort System of the Orion Module is under development.

The first full-scale test fire of the motor that powers the LAS was completed on November 20, 2008. This was the first time a LAS test has been conducted since the 1960s, when the LAS for the Apollo Program was tested.