Antares (rocket) — BrandWiki

Antares (rocket)

Overview

Antares

function	Medium-lift launch vehicle
country-origin	United States
pcost	US$472 million until 2012
cpl	US$80-85 million‡R1R‡
height	110/120: 40.5 m 130: 41.9 m 230/230+: 42.5 m
diameter	3.9 m
mass	100 series: 282000 - 296000 kg 200 series: 298000 kg
stages	2 to 3
comparable	Delta II, Atlas III, Atlas V, Falcon 9

Antares, known during early development as Taurus II, is an American expendable medium-lift launch vehicle developed by Orbital Sciences Corporation with financial support from NASA under the Commercial Orbital Transportation Services (COTS) program awarded in February 2008. It was developed alongside Orbital's automated cargo spacecraft, Cygnus, which also received COTS funding. Like other Orbital launch vehicles, Antares leveraged lower-cost, off-the-shelf parts and designs. Since 2018, the rocket has been manufactured by Northrop Grumman.

The first stage is liquid fueled, burning RP-1 (kerosene) and liquid oxygen (LOX). As Orbital had limited experience with large liquid stages, construction was subcontracted for all versions of Antares. The 100 and 200 series were built by the Ukrainian companies Pivdenne and Pivdenmash, using refurbished NK-33 engines from the Soviet N1 program on the 100 series and newly built Russian RD-181 engines on the 200 series after the loss of an Antares 130 vehicle in 2014.[3] After Russia's 2022 invasion of Ukraine ended access to these suppliers, Northrop Grumman announced the 300 series, with a first stage developed by

History

As the Space Shuttle program neared its end, NASA sought to develop new capabilities for resupplying the International Space Station (ISS). Departing from the traditional model of government-owned and operated spacecraft, the agency proposed a new approach: commercial companies would operate spacecraft, while NASA would act as a customer.

To encourage innovation, NASA offered funding through the Commercial Orbital Transportation Services (COTS) program to support the development of new spacecraft and launch vehicles. On February 19, 2008, NASA announced that it would award Orbital Sciences Corporation a COTS contract worth $171 million. Orbital was expected to invest an additional $150 million, divided between $130 million for the rocket booster and $20 million for the spacecraft.

As part of the COTS program, Orbital would be expected to conduct a successful demonstration of its rocket booster and spacecraft. If both demonstration flights were successful, Orbital would be eligible for a lucrative Commercial Resupply Service contract of $1.9 billion for eight flights to the ISS.[4]

In June 2008, it was announced that the Mid-Atlantic Regional Spaceport, formerly part of the Wallops Flight Facility, in Virginia, would be the primary launch site for the rocket.[5] Launch pad 0A (LP-0A), previously used for the failed Conestoga rocket, would be modified to handle Antares.[6] Wallops allows launches which reach the International Space Station's orbit as effectively as those from Cape Canaveral, Florida, while being less crowded.[7] The first Antares flight launched a Cygnus mass simulator.

On December 10, 2009, Alliant Techsystems Inc. (ATK) test-fired their Castor 30 motor for use on the second stage of the Antares rocket.[8] In March 2010, Orbital Sciences and Aerojet completed test firings of the AJ-26 engines.

Originally designated the Taurus II, Orbital Sciences renamed the vehicle Antares, after the star of the same name,[9] on December 12, 2011.

As of April 2012, development costs were estimated at $472 million.

On February 22, 2013, a hot fire test was successfully performed, the entire first stage being erected on the pad and held down while the engines fired for 29 seconds.

Design

First stage

The first stage of Antares burns RP-1 (kerosene) and liquid oxygen (LOX). As Orbital had little experience with large liquid stages and LOX propellant, the first stage core was designed and is manufactured in Ukraine by Pivdenne Design Office and Pivdenmash and includes propellant tanks, pressurization tanks, valves, sensors, feed lines, tubing, wiring and other associated hardware.[10] Like the Zenit—also manufactured by Pivdenmash—the Antares vehicle has a diameter of 3.9 m with a matching 3.9 m payload fairing.

Antares 100 series

The Antares 100-series first stage was powered by two Aerojet AJ26 engines. These began as Kuznetsov NK-33 engines built in the Soviet Union in the late 1960s and early 1970s, 43 of which were purchased by Aerojet in the 1990s. Twenty of these were refurbished into AJ26 engines for Antares.[11] Modifications included equipping the engines for gimballing, adding US electronics, and qualifying the engines to fire for twice as long as designed and to operate at 108% of their original thrust. Together they produced 3265 kN of thrust at sea level and 3630 kN in vacuum.

Following the catastrophic failure of an AJ26 during testing at Stennis Space Center in May 2014 and the Orb-3 launch failure in October 2014, likely caused by an engine turbopump,[12] the Antares 100-series was retired.

Antares 200 series

Because of concerns over corrosion, aging, and the limited supply of AJ26 engines, Orbital had selected new first stage engines to bid on a second major long-term contract for cargo resupply of the ISS. After the loss of the Antares rocket in October 2014, Orbital Sciences announced that the Russian RD-181—a modified version of the RD-191—would replace the AJ-26 on the Antares 200-series.[13][14] The first flight of the Antares 230 configuration using the RD-181 launched on October 17, 2016, carrying the Cygnus OA-5 cargo to the ISS.

The Antares 200 and 200+ first stages are powered by two RD-181 engines, which provide 100000 lbf more thrust than the dual AJ26 engines used on the Antares 100. Orbital adapted the existing core stage to accommodate the increased performance in the 200 Series, allowing Antares to deliver up to 6500 kg to low Earth orbit. The surplus performance of the Antares 200-series will allow Orbital to fulfill its ISS resupply contract in only four additional flights, rather than the five that would have been required with the Antares 100-series.[15][16]

Antares 300 series

In August 2022, Northrop Grumman announced that it had contracted Firefly Aerospace to build the 300-series first stage. They will also be collaborating on the in-development Eclipse launch vehicle. Eclipse and the Antares 300-series will use the same composite structures, and seven Miranda engines. The 7200 kN of thrust they provide will be substantially greater than that of the previous 200-series first stage. Northrop Grumman indicated the new first stage will substantially increase the mass capability of Antares.[17]

The announcement occurred as a result of the 2022 Russian invasion of Ukraine, which jeopardized supply chains for the previous first stages, which had been manufactured in Ukraine and used RD-181 engines from Russia.

Antares 100 series

The Antares 100-series first stage was powered by two Aerojet AJ26 engines. These began as Kuznetsov NK-33 engines built in the Soviet Union in the late 1960s and early 1970s, 43 of which were purchased by Aerojet in the 1990s. Twenty of these were refurbished into AJ26 engines for Antares.[11] Modifications included equipping the engines for gimballing, adding US electronics, and qualifying the engines to fire for twice as long as designed and to operate at 108% of their original thrust. Together they produced 3265 kN of thrust at sea level and 3630 kN in vacuum.

Following the catastrophic failure of an AJ26 during testing at Stennis Space Center in May 2014 and the Orb-3 launch failure in October 2014, likely caused by an engine turbopump,[12] the Antares 100-series was retired.

Antares 200 series

Because of concerns over corrosion, aging, and the limited supply of AJ26 engines, Orbital had selected new first stage engines to bid on a second major long-term contract for cargo resupply of the ISS. After the loss of the Antares rocket in October 2014, Orbital Sciences announced that the Russian RD-181—a modified version of the RD-191—would replace the AJ-26 on the Antares 200-series.[13][14] The first flight of the Antares 230 configuration using the RD-181 launched on October 17, 2016, carrying the Cygnus OA-5 cargo to the ISS.

The Antares 200 and 200+ first stages are powered by two RD-181 engines, which provide 100000 lbf more thrust than the dual AJ26 engines used on the Antares 100. Orbital adapted the existing core stage to accommodate the increased performance in the 200 Series, allowing Antares to deliver up to 6500 kg to low Earth orbit. The surplus performance of the Antares 200-series will allow Orbital to fulfill its ISS resupply contract in only four additional flights, rather than the five that would have been required with the Antares 100-series.[15][16]

Antares 300 series

In August 2022, Northrop Grumman announced that it had contracted Firefly Aerospace to build the 300-series first stage. They will also be collaborating on the in-development Eclipse launch vehicle. Eclipse and the Antares 300-series will use the same composite structures, and seven Miranda engines. The 7200 kN of thrust they provide will be substantially greater than that of the previous 200-series first stage. Northrop Grumman indicated the new first stage will substantially increase the mass capability of Antares.[17]

The announcement occurred as a result of the 2022 Russian invasion of Ukraine, which jeopardized supply chains for the previous first stages, which had been manufactured in Ukraine and used RD-181 engines from Russia.

Second stage

The second stage is an Orbital ATK Castor 30-series solid-fuel rocket, developed as a derivative of the Castor 120 solid motor used as Minotaur-C's first stage, itself based on a LGM-118 Peacekeeper ICBM first stage.[18] The first two flights of Antares used a Castor 30A, which was replaced by the enhanced Castor 30B for subsequent flights. The Castor 30B produces 293.4 kN average and 395.7 kN maximum thrust, and uses electromechanical thrust vector control. For increased performance, the larger Castor 30XL is available and will be used on ISS resupply flights to allow Antares to carry the Enhanced Cygnus.[19]

The Castor 30XL upper stage for Antares 230+ is being optimized for the CRS-2 contract. The initial design of the Castor 30XL was conservatively built, and after gaining flight experience it was determined that the structural component of the motor case could be lightened.

Third stage

Antares offers three optional third stages: the Bi-Propellant Third Stage (BTS), a Star 48-based third stage and an Orion 38 motor. BTS is derived from Orbital's GEOStar, a spacecraft bus and uses nitrogen tetroxide and hydrazine for propellant; it is intended to precisely place payloads into their final orbits. The Star 48-based stage uses a Star 48BV solid rocket motor and would be used for higher energy orbits. The Orion 38 is used on the Minotaur and Pegasus rockets as an upper stage.[20]

Fairing

The 3.9 m diameter, 9.9 m high fairing is manufactured by Northrop Grumman of Iuka, Mississippi, which also builds other composite structures for the vehicle, including the combined fairing adapter, dodecagon, motor cone, and interstage.[21]

NASA Commercial Resupply Services-2 : Enhancements

On January 14, 2016, NASA awarded three cargo contracts via CRS-2. Orbital ATK's Cygnus was one of these contracts.[22]

According to Mark Pieczynski, Orbital ATK Vice President, Flight Systems Group, "A further improved version [of Antares for CRS-2 contract] is in development which will include: Stage 1 core updates including structural reinforcements and optimization to accommodate increased loads. (Also) certain refinements to the RD-181 engines and CASTOR 30XL motor; and Payload accommodations improvements including a 'pop-top' feature incorporated in the fairing to allow late Cygnus cargo load and optimized fairing adapter structure".

Previously, it was understood that these planned upgrades from the Antares 230 series would create a vehicle known as the Antares 300 series. However, when asked specifically about Antares 300 series development, Mr. Pieczynski stated that Orbital ATK has "not determined to call the upgrades, we are working on, a 300 series. This is still TBD".[23]

In May 2018 the Antares program manager Kurt Eberly indicated that the upgrades will be referred to as Antares 230+.

Use of Antares 330 for future CRS flights was confirmed in reporting from Breaking Defense in June 2024. The 330 will used the same second stage, fairing, avionics and software as prior versions.[24]

Notable missions and anomalies

Antares A-ONE

Originally scheduled for 2012, the first Antares launch, designated A-ONE was conducted on April 21, 2013,[25] carrying the Cygnus Mass Simulator (a boilerplate Cygnus spacecraft) and four CubeSats contracted by Spaceflight Incorporated: Dove 1 for Cosmogia Incorporated (now Planet Labs) and three PhoneSat satellites—Alexander,[26] Graham and Bell for NASA.[27]

Prior to the launch, a 27-second test firing of the rocket's AJ26 engines was conducted successfully on February 22, 2013, following an attempt on February 13 which was abandoned before ignition.

A-ONE used the Antares 110 configuration, with a Castor 30A second stage and no third stage. The launch took place from Pad 0A of the Mid-Atlantic Regional Spaceport on Wallops Island, Virginia. LP-0A was a former Conestoga launch complex which had only been used once before, in 1995, for the Conestoga's only orbital launch attempt. Antares became the largest—and first—liquid-fuelled rocket to fly from Wallops Island, as well as the largest rocket launched by Orbital Sciences.

The first attempt to launch the rocket, on April 17, 2013, was scrubbed after an umbilical detached from the rocket's second stage, and a second attempt on April 20 was scrubbed due to high altitude winds.[28] At the third attempt on April 21, the rocket lifted off at the beginning of its launch window. The launch window for all three attempts was three hours beginning at 21:00 UTC (17:00 EDT), shortening to two hours at the start of the terminal count, and ten minutes later in the count.[29]

Cygnus CRS Orb-3

On October 28, 2014, the attempted launch of an Antares carrying a Cygnus cargo spacecraft on the Orb-3 resupply mission failed catastrophically six seconds after liftoff from Mid-Atlantic Regional Spaceport at Wallops Flight Facility, Virginia. An explosion occurred in the thrust section just as the vehicle cleared the tower, and it fell back down onto the launch pad. The range safety officer sent the destruct command just before impact.[30] There were no injuries. Orbital Sciences reported that Launch Pad 0A "escaped significant damage", though initial estimates for repairs were in the $20 million range.[31] Orbital Sciences formed an anomaly investigation board to investigate the cause of the incident. They traced it to a failure of the first stage LOX turbopump, but could not find a specific cause. However, the refurbished NK-33 engines, originally manufactured over 40 years earlier and stored for decades, were suspected as having leaks, corrosion, or manufacturing defects that had not been detected.[32] The NASA Accident Investigation Report was more direct in its failure assessment. On October 6, 2015, almost one year after the accident, Pad 0A was restored to use. Total repair costs were about $15 million.