Manufacturer | Vought |
---|---|
Country of origin | United States |
Size | |
Height | 25 metres (82 ft) |
Diameter | 1.01 metres (3 ft 4 in) |
Mass | 16,440 kilograms (36,240 lb) |
Stages | Four |
Capacity | |
Payload to LEO | |
Mass | 76 kilograms (168 lb) |
Associated rockets | |
Family | Scout |
Launch history | |
Status | Retired |
Launch sites | Wallops LA-3 Point Arguello LC-D |
Total launches | 2 |
Success(es) | 1 |
Failure(s) | 1 |
First flight | 1962-03-29 |
Last flight | 1962-04-26 |
First stage – Algol 1D | |
Powered by | 1 solid |
Maximum thrust | 440 kilonewtons (99,000 lbf) |
Burn time | 44 seconds |
Propellant | Solid |
Second stage –Castor 1A | |
Powered by | 1 solid |
Maximum thrust | 286 kilonewtons (64,000 lbf) |
Specific impulse | 247 sec |
Burn time | 27 seconds |
Propellant | Solid |
Third stage –Antares 2A | |
Powered by | 1 X-254 |
Maximum thrust | 93 kilonewtons (21,000 lbf) |
Specific impulse | 293 sec |
Burn time | 36 seconds |
Propellant | Solid |
Fourth stage –Altair 1A | |
Powered by | 1 X-248A |
Maximum thrust | 14 kilonewtons (3,100 lbf) |
Specific impulse | 255 sec |
Burn time | 40 seconds |
Propellant | Solid |
Scout X-2 was an American expendable launch system and sounding rocket which was flown twice in 1962. It was a four-stage rocket,based on the earlier Scout X-1,uprated first and third stages. It was a member of the Scout family of rockets.
The Scout X-2 used an Algol 1D first stage,instead of the earlier Algol 1B used on the Scout X-1. The third stage was the Antares 2A,a more powerful version of the Antares 1A used on earlier variants of the Scout rocket. The second and fourth stages were the same as those used on the Scout X-1;a Castor 1A and an Altair 1A respectively.
The first Scout X-2 was launched on a suborbital flight at 07:27 GMT on 29 March 1962. It flew from Launch Area 3 of the Wallops Flight Facility. The flight carried plasma and aeronomy experiments to an apogee of 6,291 kilometres (3,909 mi),and was successful. The second flight,launched on 26 April,carried the Solrad 4B satellite. It failed to reach orbit. Following this launch,the Scout X-2 was replaced by the upgraded Scout X-2M.
The Scout family of rockets were American launch vehicles designed to place small satellites into orbit around the Earth. The Scout multistage rocket was the first orbital launch vehicle to be entirely composed of solid fuel stages. It was also the only vehicle of that type until the successful launch of the Japanese Lambda 4S in 1970.
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Antares,known during early development as Taurus II,is an expendable launch system developed by Orbital Sciences Corporation and the Pivdenne Design Bureau to launch the Cygnus spacecraft to the International Space Station as part of NASA's COTS and CRS programs. Able to launch payloads heavier than 8,000 kg (18,000 lb) into low Earth orbit,Antares is the largest rocket operated by Northrop Grumman. Antares launches from the Mid-Atlantic Regional Spaceport and made its inaugural flight on April 21,2013. Antares 100 was retired in 2014 and series 200 was retired in 2023 due to component unavailability. As of January 2024 Antares 300 is under development.
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The Proton-K,also designated Proton 8K82K after its GRAU index or SL-12 after its model number,8K82K,was a Russian,previously Soviet,carrier rocket derived from the earlier Proton. It was built by Khrunichev,and launched from sites 81 and 200 at the Baikonur Cosmodrome in Kazakhstan.
The Vostok-K,GRAU index 8K72K was an expendable carrier rocket used by the Soviet Union for thirteen launches between 1960 and 1964,six of which were crewed. It was derived from the earlier Vostok-L;however,it featured uprated engines to improve performance,and enlarge its payload capacity. It was a member of the Vostok family of rockets.
The NOTS-EV-2 Caleb,also known as NOTS-500,Hi-Hoe and SIP was an expendable launch system,which was later used as a sounding rocket and prototype anti-satellite weapon. It was developed by the United States Navy's Naval Ordnance Test Station (NOTS) as a follow-up to the NOTS-EV-1 Pilot,which had been abandoned following ten launches officially classified as failed missions. Two were launched in July and October 1960,before the cancellation of the project. Following cancellation,two leftover Calebs were used in the Satellite Interceptor Program (SIP),while three more were used as sounding rockets,under the designation Hi-Hoe. These derivatives flew until July 1962,when the Hi-Hoe made its final flight.
Scout X,also known as Cub Scout,was an American rocket which served as a prototype of the Scout,which was launched on a single test flight in 1960. It was used to test the configuration that later Scout rockets would use as well as two of the solid rocket motors that would be used on them.
Scout X-1 was an American expendable launch system and sounding rocket which was flown seven times between August 1960 and October 1961. Four orbital and three suborbital launches were made,with four of the launches resulting in failures.
The RM-90 Blue Scout II was an American sounding rocket and expendable launch system which was flown three times during 1961. It was used for two HETS test flights,and the launch of the Mercury-Scout 1 satellite for NASA. It was a member of the Scout family of rockets.
The RM-89 Blue Scout I was an American sounding rocket which was flown four times between January 1961 and April 1962. It was used for two HETS test flights,and a flight to investigate atmospheric re-entry. It was a member of the Scout family of rockets.
Scout X-1A was an American sounding rocket which was flown in 1962. It was a five-stage derivative of the earlier Scout X-1,with an uprated first stage,and a NOTS-17 upper stage.
Scout X-2M was an American expendable launch system which was flown three times between May 1962 and April 1963. It was a four-stage rocket,based on the earlier Scout X-2,but with an MG-18 upper stage instead of the Altair used on the X-2. It was a member of the Scout family of rockets.
The Scout X-2B was an American expendable launch system which was flown during 1963. It was a four-stage rocket,based on the earlier Scout X-2,but with an Altair 2A fourth stage in place of the Altair 1A used on the X-2. It was a member of the Scout family of rockets.
This article compares different orbital launcher families. The article is organized into two tables:the first contains a list of currently active and under-development launcher families,while the second contains a list of retired launcher families.
This article documents notable spaceflight events during the year 2019.
The Algol family of solid-fuel rocket stages and boosters is built by Aerojet and used on a variety of launch vehicles. It was developed by Aerojet from the earlier Jupiter Senior and the Navy Polaris programs. Upgrades to the Algol motor occurred from 1960 until the retirement of the Scout launch vehicle in 1994.
A medium-lift launch vehicle (MLV) is a rocket launch vehicle that is capable of lifting between 2,000 to 20,000 kg by NASA classification or between 5,000 to 20,000 kilograms by Russian classification of payload into low Earth orbit (LEO). An MLV is between small-lift launch vehicles and heavy-lift launch vehicles.
Landmapper is a remote sensing satellite constellation built and operated by Astro Digital. It consists of two separate satellite designs:Landmapper-BC and Landmapper-HD. These satellites will be launched into Sun synchronous orbits varying in altitude between 625 km and 475 km. Both satellites are designed to CubeSat standards:6U XL for Landmapper-BC,and 16U for Landmapper-HD. They will be contained in deployers designed by Innovative Solutions in Launch of the Netherlands and ECM Launch Services of Germany. These deployers are to be included on board a variety of launch vehicles,including the SpaceX Falcon 9,Rocket Lab Electron,Glavkosmos Soyuz,Antrix PSLV,and European Space Agency Vega.