This rocket article contains payload capacity, but does not include orbital altitude or inclination , which greatly affects the capacity. |
Function | Cargo Launch Vehicle |
---|---|
Country of origin | United States |
Size | |
Height | 116 m (381 ft) or 109 m (358 ft) |
Diameter | 10 m (33 ft) or 8.4 m (28 ft) |
Mass | 3,700,000 kilograms (8,200,000 lb) RS-68 variant [1] |
Stages | 2 |
Capacity | |
Payload to LEO | |
Mass | 188,000 kg (414,000 lb) [2] |
Payload to TLI | |
Mass | 71,100 kg (156,700 lb) or 60,600 kg (133,600 lb) |
Launch history | |
Status | Canceled |
Launch sites | Kennedy,LC-39A (planned) |
Boosters | |
No. boosters | 2 ×five-segment Solid Rocket Boosters |
Height | 54 m (177 ft) |
Diameter | 3.7 m (12 ft) |
Propellant | APCP |
First stage | |
Empty mass | 140,000 kg (310,000 lb) |
Gross mass | 1,914,000 kg (4,220,000 lb) |
Powered by | |
Maximum thrust |
|
Propellant | LH2 / LOX |
Second stage –Earth Departure Stage | |
Powered by | 1 or 2 ×J-2X |
Propellant | LH2 / LOX |
The Ares V (formerly known as the Cargo Launch Vehicle or CaLV) was the planned cargo launch component of the cancelled NASA Constellation program,which was to have replaced the Space Shuttle after its retirement in 2011. Ares V was also planned to carry supplies for a human presence on Mars. [4] Ares V and the smaller Ares I were named after Ares,the Greek god of war.
The Ares V was to launch the Earth Departure Stage and Altair lunar lander for NASA's return to the Moon,which was planned for 2019. [5] It would also have served as the principal launcher for missions beyond the Earth-Moon system,including the program's ultimate goal,a crewed mission to Mars. The uncrewed Ares V would complement the smaller and human-rated Ares I rocket for the launching of the 4–6 person Orion spacecraft. Both rockets,deemed safer than the then-current Space Shuttle,would have employed technologies developed for the Apollo program,the Shuttle program,and the Delta IV EELV program. [6] However,the Constellation program,including Ares V and Ares I,was canceled in October 2010 by the NASA Authorization Act of 2010. In September 2011,NASA detailed the Space Launch System as its new vehicle for human exploration beyond Earth's orbit, [7] while commercial space companies would provide low Earth orbit access for both cargo and astronauts.
In the 1996 book The Case for Mars ,author Robert Zubrin discussed a possible future heavy launch vehicle named Ares. In the book,the rocket would have consisted of the Space Shuttle external tank powered by four Space Shuttle Main Engines (SSMEs) and a second stage powered by an RL-10 engine. One notable difference in the Zubrin et al. design is that the SSMEs were on a small side-mounted flyback craft. This design was meant to allow the Ares to fly using existing Space Shuttle infrastructure. [8]
Ares V was to be the cargo launch component of the Constellation program. Unlike the Saturn V and Space Shuttle,where the crew and cargo were launched together on the same rocket,Project Constellation planned to use two separate launch vehicles,the Ares I and the Ares V,for crew and cargo respectively. This configuration would have allowed the two launch vehicles to be optimized for their respective missions. Constellation therefore combined the Lunar Orbit Rendezvous used by Apollo with the Earth Orbit Rendezvous mode proposed by Dr. Wernher von Braun (alongside the "Direct Ascent" proposal) during the early planning stages of Apollo.
Development of the rocket and its Earth departure stage was led by NASA's Marshall Space Flight Center. NASA's Ames Research Center was responsible for the Ares V integrated health management system and for developing its payload shroud. Glenn Research Center led the development of the lunar lander ascent stage as well as Ares V power system,thrust vector control system and payload shroud. Langley Research Center had a lead role in researching Ares V aerodynamics. [9]
In 2007,NASA announced that Alliant Techsystems would be the contractor for the SRBs of both Ares I and Ares V. [10]
Although the Ares V was a medium- to long-term project,NASA planned to deploy its lift capability in a range of projects, [11] along the lines of the former Apollo Applications Program.
One proposal was to build an 8- to 16-meter Advanced Technology Large-Aperture Space Telescope [12] to be placed in the Sun/Earth L2 point. It would be a significant increase in dimension and performance over the Hubble Space Telescope and the Ares V vehicle was expected to carry this to its destination in a single launch.[ citation needed ] Future Ares V missions could also have served as a cost-effective,mass transport of construction materials for future spacecraft and missions,delivering raw materials,for example,to a Moon dock.[ citation needed ]
In May 2010,NASA planned flight demonstrations of Ares V hardware along with Ares I hardware after the scheduled upcoming Ares I-X Prime test of the Ares I five-segment SRB first stage. Several flights were listed as "Heavy Lift" test flights for testing the first stage of the Ares V simultaneously with the Ares I upper stage attached on top of the Ares V first stage. This would save both time and money in avoiding the gap between testing Ares I and Ares V hardware with limited funding. [13]
The Augustine Commission concluded that "under the FY 2010 funding profile,the Committee estimates that Ares V will not be available until the late 2020s". [14] Even if NASA had been given a $3 billion increase in funding and the ISS had been retired in 2015,the committee still believed that the Ares V would not be ready until the mid-2020s. [15]
On February 1,2010,President Barack Obama announced a proposal to cancel the Constellation program effective with the U.S. 2011 fiscal year budget, [16] but later announced changes to the proposal in a major space policy speech at Kennedy Space Center on April 15,2010. In October 2010,the NASA Authorization Act of 2010 was signed into law,which canceled Constellation. [17] However,previous legislation kept Constellation contracts in force until a new funding bill was passed for 2011. [18] [19] Due to previous legislative obligations,$500 million was to be paid to contractors after the program's cancellation until March 2011. [20]
This section needs additional citations for verification .(February 2020) |
The successor to the Ares rocket family is the Space Launch System,a more versatile vehicle designed to launch both crew and cargo,similar to the Ares IV concept. It has a payload range of 95-130 tons to LEO across its different variants. The SLS is similar to earlier Ares V designs in that it uses a stretched 8.4–meter external tank and is powered by 4 RS-25s. Initial designs for the SLS used the same Earth Departure Stage but development was put on hold with the 4-RL-10 Exploration Upper Stage taking its place. Both vehicles make use of the same 5–segment SRBs,although the SLS will not recover them. Under the Artemis program,the vehicle will transport crew to the Moon in the Orion spacecraft as well as logistics equipment and cargo for surface missions. They will rendezvous with a separate lunar lander either docked to the Lunar Gateway,a lunar orbital station,or free flying in lunar orbit. The SLS Block 1B version is capable of Earth orbital rendezvous lunar mission profiles such as that of the Ares V,lunar orbital rendezvous such as what NASA is currently pursuing,and integrated lunar missions such as the Apollo missions using the Saturn V,which has been proposed under a new House of Representatives bill. [21] [22] [23] [24] [25]
The Ares V was intended as a heavy launch vehicle to send large hardware and materials to the Moon,or to send supplies beyond Earth orbit to sustain human presence there. [3] The Ares V was designed to be a three-stage rocket:the first and second stages,which burn together,were to use both solid and liquid propulsion with the upper stage providing the necessary propulsion to send the hardware and staples beyond low Earth orbit and onto a trajectory to the Moon.
Ares V underwent a preliminary design review after the results of the 2009 Augustine Commission. [26] Like the Space Shuttle,the Ares vehicle was to use a pair of solid-fuel first-stage rocket boosters that burn simultaneously with the liquid-fueled core stage. The solid rocket booster on Ares V was first envisioned as an improved version of the Space Shuttle Solid Rocket Booster,but with five or five and a half segments instead of the four segments used with the Space Shuttle. [3] [27] [28] The liquid-fueled core stage was to be derived from the Space Shuttle external tank and was to use either five or six RS-68B engines attached to the bottom of a new 10 m diameter tank,or five SSMEs attached to the bottom of a stretched version of the Space Shuttle's 8.4 m external tank. It was to be fueled by liquid oxygen (LOX) and liquid hydrogen (LH2). [29]
The upper stage,derived from the S-IVB upper stage used on the Saturn IB and Saturn V rockets,was named the Earth Departure Stage (EDS). The EDS would be powered by an Apollo-derived J-2X rocket engine,which was also to be used on the liquid-fueled upper stage of the Ares I booster. The EDS was to be used to steer the Altair lunar lander into its initial low Earth "parking" orbit for later retrieval by the Orion spacecraft,and then would propel both the Altair and Orion to the Moon. [3] The EDS could also have been used to take large payloads into low Earth orbit,along with placing large uncrewed spacecraft onto trajectories beyond the Earth-Moon system.
The Ares V was designed to have a payload capacity of over 414,000 lb (188 metric tons) to Low Earth orbit (LEO),and 157,000 lb (71 metric tons) to the Moon. [3] Upon completion the Ares V would be the most powerful rocket ever built,lifting more into orbit than even the American Saturn V,the failed Soviet N-1 for the canceled Soviet Moonshot,and the successful Soviet/Russian Energia booster developed for the Buran Shuttle. [30] Besides its lunar role, [3] it could also support a crewed Orion expedition to a Near-Earth asteroid,and could boost an 8 to 16-meter successor of the Hubble Space Telescope to the Sun-Earth L2 point.
The Ares IV concept combines an Ares I upper stage on top of an Ares V. [31] Specifically,the vehicle would consist of the liquid-fueled core stage from the Ares V design,two five-segment solid rocket boosters,and the liquid-fueled upper stage from the Ares I,as described by NASA in January 2007. The Ares IV would be a combined 367 ft (112 m) tall and could be used to reach the Moon. Total payload capacity would be 90,420 lb (41,000 kg) to 240 miles (390 km) for direct trans-lunar injection. [32]
NASA had considered using Ares IV to evaluate high-speed "skip" reentry profiles of the Orion capsule in 2007. [33] NASA had planned flight demonstrations of Ares I and Ares V hardware in "Heavy Lift" configurations beginning in 2013. The "Heavy Lift" test flights were to test the first stage of the Ares V simultaneously with the Ares I upper stage attached on top to save both time and money. The later Heavy Lift test vehicle configurations are similar to the Ares IV vehicle. [34]
Ares V Lite was an alternative launch vehicle for NASA's Constellation program suggested by the Augustine Commission. Ares V Lite was a scaled down Ares V. [35] [36] It would have used five RS-68 engines and two five-segment SRBs and have had a low Earth orbit payload of approximately 140 metric tons (309,000 lb). [37] If chosen,Ares V Lite would have replaced the Ares V and Ares I launchers. One Ares V Lite version would have been a cargo lifter like Ares V and the second version would have carried astronauts in the Orion spacecraft. [37]
In the 2013 film Star Trek Into Darkness ,a desktop model of the Ares V rocket was set decoration in the office of Admiral Alexander Marcus as part of his spaceflight collection. [38]
The Space Shuttle program was the fourth human spaceflight program carried out by the U.S. National Aeronautics and Space Administration (NASA),which accomplished routine transportation for Earth-to-orbit crew and cargo from 1981 to 2011. Its official program name was Space Transportation System (STS),taken from a 1969 plan for a system of reusable spacecraft where it was the only item funded for development,as a proposed nuclear shuttle in the plan was cancelled in 1972. It flew 135 missions and carried 355 astronauts from 16 countries,many on multiple trips.
The Constellation program was a crewed spaceflight program developed by NASA,the space agency of the United States,from 2005 to 2009. The major goals of the program were "completion of the International Space Station" and a "return to the Moon no later than 2020" with a crewed flight to the planet Mars as the ultimate goal. The program's logo reflected the three stages of the program:the Earth (ISS),the Moon,and finally Mars—while the Mars goal also found expression in the name given to the program's booster rockets:Ares. The technological aims of the program included the regaining of significant astronaut experience beyond low Earth orbit and the development of technologies necessary to enable sustained human presence on other planetary bodies.
The Space Shuttle Solid Rocket Booster (SRB) was the first solid-propellant rocket to be used for primary propulsion on a vehicle used for human spaceflight. A pair of these provided 85% of the Space Shuttle's thrust at liftoff and for the first two minutes of ascent. After burnout,they were jettisoned and parachuted into the Atlantic Ocean where they were recovered,examined,refurbished,and reused.
The Space Shuttle external tank (ET) was the component of the Space Shuttle launch vehicle that contained the liquid hydrogen fuel and liquid oxygen oxidizer. During lift-off and ascent it supplied the fuel and oxidizer under pressure to the three RS-25 main engines in the orbiter. The ET was jettisoned just over 10 seconds after main engine cut-off (MECO) and it re-entered the Earth's atmosphere. Unlike the Solid Rocket Boosters,external tanks were not re-used. They broke up before impact in the Indian Ocean,away from shipping lanes and were not recovered.
The RS-25,also known as the Space Shuttle Main Engine (SSME),is a liquid-fuel cryogenic rocket engine that was used on NASA's Space Shuttle and is used on the Space Launch System (SLS).
The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown.
Shuttle-derived vehicles (SDV) are space launch vehicles and spacecraft that use components,technology,and infrastructure originally developed for the Space Shuttle program.
The Exploration Systems Architecture Study (ESAS) is the official title of a large-scale,system level study released by the National Aeronautics and Space Administration (NASA) in November 2005 of his goal of returning astronauts to the Moon and eventually Mars—known as the Vision for Space Exploration. The Constellation Program was cancelled in 2010 by the Obama Administration and replaced with the Space Launch System,later renamed as the Artemis Program in 2017 under the Trump Administration.
The Altair spacecraft,previously known as the Lunar Surface Access Module or LSAM,was the planned lander spacecraft component of NASA's cancelled Constellation program. Astronauts would have used the spacecraft for landings on the Moon,which was intended to begin around 2019. The Altair spacecraft was planned to be used both for lunar sortie and lunar outpost missions.
The Earth Departure Stage (EDS) is the name given to the proposed second stage of the Block 2 Space Launch System. The EDS is intended to boost the rocket's payload into a parking orbit around the Earth and from there send the payload out of low Earth orbit to its destination in a manner similar to that of the S-IVB rocket stage used on the Saturn V rockets that propelled the Apollo spacecraft to the Moon. Its development has been put on hold until stages capable of transferring heavy payloads to Mars are required.
Ares I was the crew launch vehicle that was being developed by NASA as part of the Constellation program. The name "Ares" refers to the Greek deity Ares,who is identified with the Roman god Mars. Ares I was originally known as the "Crew Launch Vehicle" (CLV).
The Saturn V is a retired American super heavy-lift launch vehicle developed by NASA under the Apollo program for human exploration of the Moon. The rocket was human-rated,had three stages,and was powered by liquid fuel. Flown from 1967 to 1973,it was used for nine crewed flights to the Moon,and to launch Skylab,the first American space station.
The Shuttle-Derived Heavy Lift Launch Vehicle ("HLV") was an alternate super heavy-lift launch vehicle proposal for the NASA Constellation program. It was first presented to the Augustine Commission on 17 June 2009.
DIRECT was a late-2000s proposed alternative super heavy lift launch vehicle architecture supporting NASA's Vision for Space Exploration that would replace the space agency's planned Ares I and Ares V rockets with a family of Shuttle-Derived Launch Vehicles named "Jupiter". It was intended to be the alternative to the Ares I and Ares V rockets which were under development for the Constellation program,intended to develop the Orion spacecraft for use in Earth orbit,the Moon,and Mars.
The retirement of NASA's Space Shuttle fleet took place from March to July 2011. Discovery was the first of the three active Space Shuttles to be retired,completing its final mission on March 9,2011;Endeavour did so on June 1. The final shuttle mission was completed with the landing of Atlantis on July 21,2011,closing the 30-year Space Shuttle program.
The Space Launch System (SLS) is an American super heavy-lift expendable launch vehicle used by NASA. As the primary launch vehicle of the Artemis Moon landing program,SLS is designed to launch the crewed Orion spacecraft on a trans-lunar trajectory. The first SLS launch was the uncrewed Artemis 1,which took place on 16 November 2022.
Artemis I,formerly Exploration Mission-1 (EM-1),was an uncrewed Moon-orbiting mission. As the first major spaceflight of NASA's Artemis program,Artemis I marked the agency's return to lunar exploration after the conclusion of the Apollo program five decades earlier. It was the first integrated flight test of the Orion spacecraft and Space Launch System (SLS) rocket,and its main objective was to test the Orion spacecraft,especially its heat shield,in preparation for subsequent Artemis missions. These missions seek to reestablish a human presence on the Moon and demonstrate technologies and business approaches needed for future scientific studies,including exploration of Mars.
A super heavy-lift launch vehicle is a rocket that can lift to low Earth orbit a "super heavy payload",which is defined as more than 50 metric tons (110,000 lb) by the United States and as more than 100 metric tons (220,000 lb) by Russia. It is the most capable launch vehicle classification by mass to orbit,exceeding that of the heavy-lift launch vehicle classification.
The Artemis program is a Moon exploration program led by the United States' National Aeronautics and Space Administration (NASA),formally established in 2017 via Space Policy Directive 1. It is intended to reestablish a human presence on the Moon for the first time since the Apollo 17 mission in 1972. The program's stated long-term goal is to establish a permanent base on the Moon to facilitate human missions to Mars.
During the lifetime of the Space Shuttle,Rockwell International and many other organizations studied various Space Shuttle designs. These involved different ways of increasing cargo and crew capacity,as well as investigating further reusability. A large focus of these designs were related to developing new shuttle boosters and improvements to the central tank,but also looked to expand NASA's ability to launch deep space missions and build modular space stations. Many of these concepts and studies would shape the concepts and programs of the 2000s such as the Constellation,Orbital Space Plane Program,and Artemis program.
This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration .