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Pegasus is an air-launched multistage rocket developed by Orbital Sciences Corporation (OSC) and later built and launched by Northrop Grumman. Pegasus is the world's first privately developed orbital launch vehicle. [2] [3] Capable of carrying small payloads of up to 443 kg (977 lb) into low Earth orbit, Pegasus first flew in 1990 and remained active as of 2021 [update] . The vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 12,000 m (39,000 ft) using a first stage wing and a tail to provide lift and altitude control while in the atmosphere. The first stage does not have a thrust vector control (TVC) system. [4]
Pegasus was designed by a team led by Antonio Elias. [5] The Pegasus's three Orion solid motors were developed by Hercules Aerospace (later Alliant Techsystems) specifically for the Pegasus launcher but using advanced carbon fiber, propellant formulation and case insulation technologies originally developed for the terminated USAF Small ICBM program. The wing and fins' structures were designed by Burt Rutan and his company, Scaled Composites, which manufactured them for Orbital.
Started in the spring of 1987, [6] the development project was funded by Orbital Sciences Corporation and Hercules Aerospace, and did not receive any government funding. Government funding was received to support operational testing. [7] NASA did provide the use of the B-52 carrier aircraft on a cost-reimbursable basis during the development (captive carry tests) and the first few flights. Two Orbital internal projects, the Orbcomm communications constellation and the OrbView observation satellites, served as anchor customers to help justify the private funding. [8]
There were no Pegasus test launches prior to the first operational launch on 5 April 1990 with NASA test pilot and former astronaut Gordon Fullerton in command of the carrier aircraft. Initially, a NASA-owned B-52 Stratofortress NB-008 served as the carrier aircraft. By 1994, Orbital had transitioned to their "Stargazer" L-1011, a converted airliner which was formerly owned by Air Canada. The name "Stargazer" is an homage to the television series Star Trek: The Next Generation : the character Jean-Luc Picard was captain of a ship named Stargazer prior to the events of the series, and his first officer William Riker once served aboard a ship named Pegasus . [9]
During its 45-launch history, the Pegasus program had three mission failures (STEP-1, STEP-2 and HETI/SAC-B), and two partial failures, (USAF Microsat and STEP-2) followed by 30 consecutive successful flights for a total program success rate of 89 percent. [10] The first partial failure on 17 July 1991 caused the seven USAF microsatellites to be delivered to a lower than planned orbit, significantly reducing the mission lifetime. The last mission failure on 4 November 1996 resulted in the loss of gamma-burst identifying satellite HETE (High Energy Transient Explorer). [11]
The Pegasus XL, introduced in 1994 has lengthened stages to increase payload performance. [12] In the Pegasus XL, the first and second stages are lengthened into the Orion 50SXL and Orion 50XL, respectively. Higher stages are unchanged; flight operations are similar. The wing is strengthened slightly to handle the higher weight. The standard Pegasus has been discontinued; the Pegasus XL is still active as of 2019. Pegasus has flown 44 missions in both configurations, launching 91 satellites as of October 12, 2019. [13] [14]
Dual payloads can be launched, with a canister that encloses the lower spacecraft and mounts the upper spacecraft. The upper spacecraft deploys, the canister opens, then the lower spacecraft separates from the third-stage adapter. Since the fairing is unchanged for cost and aerodynamic reasons, each of the two payloads must be relatively compact. Other multiple-satellite launches involve "self-stacking" configurations, such as the ORBCOMM spacecraft.
For their work in developing the rocket, the Pegasus team led by Antonio Elias was awarded the 1991 National Medal of Technology by U.S. President George H. W. Bush.
The initial launch price offered was US$6 million, without options or a HAPS (Hydrazine Auxiliary Propulsion System) maneuvering stage. With the enlargement to Pegasus XL and the associated improvements to the vehicle, baseline prices increased. In addition, customers usually purchase additional services, such as extra testing, design and analysis, and launch-site support. [15]
As of 2015, the most recent Pegasus XL to be purchased — a planned June 2017 launch of NASA's Ionospheric Connection Explorer (ICON) mission — had a total cost of US$56.3 million, which NASA notes includes "firm-fixed launch service costs, spacecraft processing, payload integration, tracking, data and telemetry and other launch support requirements". [15] A series of technical problems delayed this launch, which finally took place on 11 October 2019.
In July 2019, it was announced that Northrop Grumman had lost the launch contract of the Imaging X-ray Polarimetry Explorer (IXPE) satellite to SpaceX. IXPE had been planned to be launched by a Pegasus XL rocket, and had been designed so as to fit within the Pegasus XL rocket constraints. With the IXPE launch removed from the Pegasus XL rocket, there are currently (as of 12 October 2019, after the launch of ICON) no space launch missions announced for the Pegasus XL rocket. The future (under construction as of 2019) NASA Explorer program mission Polarimeter to Unify the Corona and Heliosphere (PUNCH) was planned to be launched by Pegasus XL; but then NASA decided to merge the launches of PUNCH and another Explorer mission, Tandem Reconnection and Cusp Electrodynamics Reconnaissance Satellites (TRACERS) (also under construction as of 2019). These two space missions, consisting of 6 satellites in total, are to be launched by one launch vehicle. It is expected that a larger launcher will be chosen for this dual mission launch. [16] In August 2022 NASA announced that the 4 microsatellites of the PUNCH constellation will be launched as rideshare payloads together with SPHEREx in April 2025 on a SpaceX Falcon 9 rocket. [17] [18] SpaceX's internal launch cost for a reusable Falcon 9 rocket is less than $20 million, [19] while having vastly larger payload capacity, so it seems likely that SpaceX would be able to profitably underbid the Pegasus XL for most satellite launches.
Northrop has one Pegasus XL remaining in its inventory. It is looking for customers for those rockets. Northrop does not plan on retiring the Pegasus XL rocket as of October 2019. [20]
In a Pegasus launch, the carrier aircraft takes off from a runway with support and checkout facilities. Such locations have included Kennedy Space Center / Cape Canaveral Air Force Station, Florida; Vandenberg Air Force Base and Dryden Flight Research Center, California; Wallops Flight Facility, Virginia; Kwajalein Range in the Pacific Ocean, and the Canary Islands in the Atlantic Ocean. Orbital offers launches from Alcantara, Brazil, but no known customers have performed any.
Upon reaching a predetermined staging time, location, and velocity the aircraft releases the Pegasus. After five seconds of free-fall, the first stage ignites and the vehicle pitches up. The 45-degree delta wing (of carbon composite construction and double-wedge airfoil) aids pitch-up and provides some lift. The tail fins provide steering for first-stage flight, as the Orion 50S motor does not have a thrust-vectoring nozzle.
Approximately 1 minute and 17 seconds later, the Orion 50S motor burns out. The vehicle is at over 200,000 feet (61 km) in altitude and hypersonic speed. The first stage falls away, taking the wing and tail surfaces, and the second stage ignites. The Orion 50 burns for approximately 1 minute and 18 seconds. Attitude control is by thrust vectoring the Orion 50 motor around two axes, pitch and yaw; roll control is provided by nitrogen thrusters on the third stage.[ citation needed ]
Midway through second-stage flight, the launcher has reached a near-vacuum altitude. The fairing splits and falls away, uncovering the payload and third stage. Upon burnout of the second-stage motor, the stack coasts until reaching a suitable point in its trajectory, depending on mission. Then the Orion 50 is discarded, and the third stage's Orion 38 motor ignites. It too has a thrust-vectoring nozzle, assisted by the nitrogen thrusters for roll. After approximately 64 seconds, the third stage burns out.[ citation needed ]
A fourth stage is sometimes added for a higher altitude, finer altitude accuracy, or more complex maneuvers. The HAPS (Hydrazine Auxiliary Propulsion System) is powered by three restartable, monopropellant hydrazine thrusters. As with dual launches, the HAPS cuts into the fixed volume available for payload. In at least one instance, the spacecraft was built around the HAPS.
Guidance is via a 32-bit computer and an IMU. A GPS receiver gives additional information. Due to the air launch and wing lift, the first-stage flight algorithm is custom-designed. The second- and third-stage trajectories are ballistic, and their guidance is derived from a Space Shuttle algorithm.[ citation needed ]
The carrier aircraft (initially a NASA B-52, now an L-1011 owned by Northrop Grumman) serves as a booster to increase payloads at reduced cost. 12,000 m (39,000 ft) is only about 4% of a low Earth orbital altitude, and the subsonic aircraft reaches only about 3% of orbital velocity, yet by delivering the launch vehicle to this speed and altitude, the reusable aircraft replaces a costly first-stage booster.
In October 2016, Orbital ATK announced a partnership with Stratolaunch Systems to launch Pegasus-XL rockets from the giant Scaled Composites Stratolaunch, which could launch up to three Pegasus-XL rockets on a single flight. [21]
Pegasus components have also been the basis of other Orbital Sciences Corporation launchers. [22] The ground-launched Taurus rocket places the Pegasus stages and a larger fairing atop a Castor 120 first stage, derived from the first stage of the MX Peacekeeper missile. Initial launches used refurbished MX first stages.
The Minotaur I, also ground-launched, is a combination of stages from Taurus launchers and Minuteman missiles, hence the name. The first two stages are from a Minuteman II; the upper stages are Orion 50XL and 38. Due to the use of surplus military rocket motors, it is only used for U.S. Government and government-sponsored payloads.[ why? ]
A third vehicle is dubbed Minotaur IV despite containing no Minuteman stages. It consists of a refurbished MX with an Orion 38 added as a fourth stage.
The NASA X-43A hypersonic test vehicles were boosted by Pegasus first stages. The upper stages were replaced by exposed models of a scramjet-powered vehicle. The Orion stages boosted the X-43 to its ignition speed and altitude, and were discarded. After firing the scramjet and gathering flight data, the test vehicles also fell into the Pacific.
The most numerous derivative of Pegasus is the booster for the Ground-based Midcourse Defense (GBMD) interceptor, basically a vertical (silo) launched Pegasus minus wing and fins, and with the first stage modified by addition of a Thrust Vector Control (TVC) system.
Pegasus has flown 45 missions between 1990 and 2021. [13]
Flight No. | Date / time (UTC) | Rocket, Configuration | Launch site | Payload | Payload mass | Target Orbit [23] | Actual Orbit [23] | Customer | Launch outcome |
---|---|---|---|---|---|---|---|---|---|
1 | 5 April 1990 19:10:17 | Standard (B-52) | Edwards AFB | Pegsat, NavySat | 320.0 x 360.0 km @ 94.00° i | 273.0 x 370.0 km @ 94.15° i | Success | ||
2 | 17 July 1991 17:33:53 | Standard w/ HAPS (B-52) | Edwards AFB | Microsats (7 satellites) | 389.0 x 389.0 km @ 82.00° i | 192.4 x 245.5 km @ 82.04° i | Partial failure | ||
Orbit too low, spacecraft reentered after 6 months instead of planned 3-years lifetime. | |||||||||
3 | 9 February 1993 14:30:34 | Standard (B-52) | Kennedy Space Center | SCD-1 | 405.0 x 405.0 km @ 25.00° i | 393.0 x 427.0 km @ 24.97° i | Success | ||
In the final minute of the launch sequence an abort was called by NASA's Range Safety Officer (RSO). Despite the abort call, the launch was reinitiated by then operator Orbital Sciences Corporation's test conductor without coordination with other launch participants. [24] [25] Launch was completed without further issue. In an investigation led by the National Transportation Safety Board (NTSB) found that: fatigue; lack of clear command, control, and communication roles were factors that led to the incident. [25] | |||||||||
4 | 25 April 1993 13:56:00 | Standard (B-52) | Edwards AFB | ALEXIS – Array of Low Energy X-ray Imaging Sensors | 400.0 x 400.0 km @ 70.00° i | 404.0 x 450.5 km @ 69.92° i | Success | ||
5 | 19 May 1994 17:03 | Standard w/ HAPS (B-52) | Edwards AFB | STEP-2 (Space Test Experiments Platform/Mission 2/SIDEX) | 450.0 x 450.0 km @ 82.00° i | 325.0 x 443.0 km @ 81.95° i | Partial failure | ||
Orbit slightly low | |||||||||
6 | 27 June 1994 21:15 | XL (L-1011) | Vandenberg AFB | STEP-1 (Space Test Experiments Platform/Mission 1) | - | - | Failure | ||
Loss of vehicle control 35 seconds into flight, flight terminated. | |||||||||
7 | 3 August 1994 14:38 | Standard (B-52) | Edwards AFB | APEX | 195.0 x >1000 km @ 70.02° i | 195.5 x 1372.0 km @ 69.97° i | Success | ||
8 | 3 April 1995 13:48 | Hybrid (L-1011) [lower-alpha 1] | Vandenberg AFB | Orbcomm (2 satellites), OrbView 1 | 398.0 x 404.0 km @ 70.00° i | 395.0 x 411.0 km @ 70.03° i | Success | ||
9 | 22 June 1995 19:58 | XL (L-1011) | Vandenberg AFB | STEP-3 (Space Test Experiments Platform/Mission 3) | - | - | Failure | ||
Destroyed during second-stage flight | |||||||||
10 | 9 March 1996 01:33 | XL (L-1011) | Vandenberg AFB | REX II | 450.0 x 443.0 km @ 90.00° i | 450.9 x 434.3 km @ 89.96° i | Success | ||
11 | 17 May 1996 02:44 | Hybrid (L-1011) | Vandenberg AFB | MSTI-3 | 298.0 x 394.0 km @ 97.13° i | 293.0 x 363.0 km @ 97.09° i | Success | ||
12 | 2 July 1996 07:48 | XL (L-1011) | Vandenberg AFB | TOMS-EP | 340.0 x 955.0 km @ 97.40° i | 341.2 x 942.9 km @ 97.37° i | Success | ||
13 | 21 August 1996 09:47:26 | XL (L-1011) | Vandenberg AFB | FAST (Fast Auroral Snapshot Explorer) | 350.0 x 4200.0 km @ 83.00° i | 350.4 x 4169.6 km @ 82.98° i | Success | ||
14 | 4 November 1996 17:08:56 | XL (L-1011) | Wallops Flight Facility | HETE, SAC-B | 510.0 x 550.0 km @ 38.00° i | 488.1 x 555.4 km @ 37.98° i | Failure | ||
Satellites not ejected from third stage | |||||||||
15 | 21 April 1997 11:59:06 | XL (L-1011) | Gando Air Base, Gran Canaria, Spain | Minisat 01, Celestis space burial | 587.0 x 587.0 km @ 151.01° i | 562.6 x 581.7 km @ 150.97° i | Success | ||
16 | August 1, 1997 20:20:00 | XL (L-1011) | Vandenberg AFB | OrbView-2 | 310.0 x 400.0 km @ 98.21° i | 300.0 x 302.0 km @ 98.28° i | Success | ||
On the line with partial success | |||||||||
17 | August 29, 1997 15:02:00 | XL (L-1011) | Vandenberg AFB | FORTE | 800.0 x 800.0 km @ 70.00° i | 799.9 x 833.4 km @ 69.97° i | Success | ||
18 | October 22, 1997 13:13:00 | XL (L-1011) | Wallops Flight Facility | STEP-4 (Space Test Experiments Platform/Mission 4) | 430.0 x 510.0 km @ 45.00° i | 430.0 x 511.0 km @ 44.98° i | Success | ||
19 | December 23, 1997 19:11:00 | XL w/ HAPS (L-1011) | Wallops Flight Facility | Orbcomm (8 satellites) | 825.0 x 825.0 km @ 45.00° i | 822.0 x 824.0 km @ 45.02° i | Success | ||
20 | February 26, 1998 07:07:00 | XL (L-1011) | Vandenberg AFB | SNOE, BATSAT | 580.0 x 580.0 km @ 97.75° i | 582.0 x 542.0 km @ 97.76° i | Success | ||
21 | April 2, 1998 02:42:00 | XL (L-1011) | Vandenberg AFB | TRACE | 600.0 x 650.0 km @ 97.88° i | 599.9 x 649.2 km @ 97.81° i | Success | ||
22 | August 2, 1998 16:24:00 | XL w/ HAPS (L-1011) | Wallops Flight Facility | Orbcomm (8 satellites) | 818.5 x 818.5 km @ 45.02° i | 819.5 x 826.0 km @ 45.01° i | Success | ||
23 | September 23, 1998 05:06:00 | XL w/ HAPS (L-1011) | Wallops Flight Facility | Orbcomm (8 satellites) | 818.5 x 818.5 km @ 45.02° i | 811.0 x 826.0 km @ 45.02° i | Success | ||
24 | October 22, 1998 00:02:00 | Hybrid (L-1011) | Cape Canaveral | SCD-2 | 750.0 x 750.0 km @ 25.00° i | 750.4 x 767.0 km @ 24.91° i | Success | ||
25 | December 6, 1998 00:57:00 | XL (L-1011) | Vandenberg AFB | SWAS | 635.0 x 700.0 km @ 70.00 ° i | 637.7 x 663.4 km @ 69.91° i | Success | ||
26 | March 5, 1999 02:56:00 | XL (L-1011) | Vandenberg AFB | WIRE – Wide Field Infrared Explorer | 540.0 x 540.0 km @ 97.56° i | 539.0 x 598.0 km @ 97.53° i | Success | ||
27 | May 18, 1999 05:09:00 | XL w/ HAPS (L-1011) | Vandenberg AFB | Terriers, MUBLCOM | 550.0 x 550.0 km @ 97.75° i, 775.0 x 775.0 km @ 97.75° i | 551.0 x 557.0 km @ 97.72° i, 774.0 x 788.0 km @ 97.72° i | Success | ||
28 | December 4, 1999 18:53:00 | XL w/ HAPS (L-1011) | Wallops Flight Facility | Orbcomm (7 satellites) | 825.0 x 825.0 km @ 45.02° i | 826.5 x 829.0 km @ 45.02° i | Success | ||
29 | June 7, 2000 13:19:00 | XL (L-1011) | Vandenberg AFB | TSX-5 (Tri-Service-Experiments mission 5) | 405.0 x 1.750.0 km @ 69.00° i | 409.9 x 1,711.7 km @ 68.95° i | Success | ||
30 | October 9, 2000 05:38:00 | Hybrid (L-1011) | Kwajalein Atoll | HETE 2 | 600.0 x 650.0 km @ 2.00° i | 591.9 x 651.9 km @ 1.95° i | Success | ||
31 | February 5, 2002 20:58:00 | XL (L-1011) | Cape Canaveral | RHESSI | 600.0 x 600.0 km @ 38.00° i | 586.4 x 602.0 km @ 38.02° i | Success | ||
32 | January 25, 2003 20:13:00 | XL (L-1011) | Cape Canaveral | SORCE | 645.0 x 645.0 km @ 40.00° i | 622.3 x 647.3 km @ 39.999° i | Success | ||
33 | April 28, 2003 11:59:00 | XL (L-1011) | Cape Canaveral | GALEX – Galaxy Evolution Explorer | 690.0 x 690.0 km @ 29.00° i | 689.8 x 711.3 km @ 28.99° i | Success | ||
34 | June 26, 2003 18:53:00 | XL (L-1011) | Vandenberg AFB | OrbView-3 | 369.0 x 470.0 km @ 97.29° i | 367.1 x 440.5 km @ 97.27° i | Success | ||
35 | August 13, 2003 02:09:00 | XL (L-1011) | Vandenberg AFB | SCISAT-1 | 650.0 x 650.0 km @ 73.92° i | 647.9 x 659.7 km @ 73.95° i | Success | ||
36 | April 15, 2005 17:26:00 | XL w/ HAPS (L-1011) | Vandenberg AFB | DART | 538.7 x 566.7 km @ 97.73° i | 541.2 x 548.8 km @ 97.73° i | Success | ||
37 | March 22, 2006 14:03:00 | XL (L-1011) | Vandenberg AFB | ST-5 – Space Technology 5 (3 satellites) | 300.0 x 4500.0 km @ 105.6° i | 301.1 x 4571.0 km @ 105.62° i | Success | ||
38 | April 25, 2007 20:26:00 | XL (L-1011) | Vandenberg AFB | AIM – Aeronomy of Ice in the Mesosphere | 197 kg (434 lb) [27] | 600.0 x600.0 km @ 97.77° i | 601.3 x 596.2 km @ 97.79° i | NASA [27] | Success |
39 | April 16, 2008 17:02:00 | XL (L-1011) | Kwajalein Atoll | C/NOFS | 384 kg (847 lb) [28] | 400.0 x 850.0 km @ 13.0° i | 401.0 x 868.0 km @ 12.99° i | STP / AFRL / DMSG [28] | Success |
40 | October 19, 2008 17:47:23 | XL (L-1011) | Kwajalein Atoll | IBEX – Interstellar Boundary Explorer | 107 kg (236 lb) [29] | 207.0 x 412.0 km @11.0° i | 206.4 x 445.0 km @ 10.99° i | NASA | Success |
41 | June 13, 2012 16:00:00 | XL (L-1011) | Kwajalein Atoll | NuSTAR – Nuclear Spectroscopic Telescope Array | 350 kg (770 lb) [30] | ≥530.0 x ≤660.0 km @ 5.0 – 7.0° i | 621.2 x 638.5 km @ 6.024° i | NASA / JPL | Success [31] |
42 | June 28, 2013 02:27:46 [32] | XL (L-1011) | Vandenberg AFB | IRIS – Interface Region Imaging Spectrograph SMEX | 183 kg (403 lb) [33] | ≥620.0 x ≤670.0 km @97.89° i | 622.9 x 669.3 km @ 97.894° i | NASA | Success [33] |
43 | December 15, 2016 13:37:00 | XL (L-1011) | Cape Canaveral | Cyclone Global Navigation Satellite System (CYGNSS) [34] | 345.6 kg (762 lb) [35] | 510.0 x 6888.0 km @ 35° i | 511.5 x 6908.1 km @ 34.97° i | NASA | Success [36] |
44 | 11 October 2019 01:59:05 | XL (L-1011) | Cape Canaveral | Ionospheric Connection Explorer (ICON) | 281 kg (619 lb) [37] [38] | LEO, 590 x 607 km [38] | 608.4 x 571.6 @ 26.98° i | UC Berkeley SSL / NASA | Success [39] |
45 | 13 June 2021 08:11 [40] [41] | XL (L-1011) | Vandenberg Space Force Base | TacRL-2 (Odyssey) | 325 kg (717 lb) | LEO - | U.S. Space Force | Success [42] | |
Orbital Sciences Corporation was an American company specializing in the design, manufacture, and launch of small- and medium- class space and launch vehicle systems for commercial, military and other government customers. In 2014, Orbital merged with Alliant Techsystems (ATK) to create a new company called Orbital ATK, which in turn was purchased by Northrop Grumman in 2018.
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Minotaur-C, formerly known as Taurus or Taurus XL, is a four stage solid fueled launch vehicle built in the United States by Orbital Sciences and launched from SLC-576E at California's Vandenberg Air Force Base. It is based on the air-launched Pegasus rocket from the same manufacturer, utilizing a "zeroth stage" in place of an airplane. The Minotaur-C is able to carry a maximum payload of around 1458 kg into a low Earth orbit (LEO).
The Minotaur is a family of United States solid-fuel launch vehicles repurposed from retired Minuteman and Peacekeeper model intercontinental ballistic missiles. Built by Northrop Grumman under the Space Force's Rocket Systems Launch Program, these vehicles are used for various space and test launch missions.
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Antares, known during early development as Taurus II, is an American expendable medium-lift launch vehicle developed and built by Orbital Sciences Corporation with financial support from NASA under the Commercial Orbital Transportation Services (COTS) program awarded in February 2008, alongside the company's automated cargo spacecraft, Cygnus. Like other launch vehicles developed by Orbital, Antares leveraged lower-cost, off-the-shelf parts and designs.
This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets. For the simple list of all conventional launcher families, see: Comparison of orbital launchers families. For the list of predominantly solid-fueled orbital launch systems, see: Comparison of solid-fueled orbital launch systems.
Cygnus is an expendable American automated cargo spacecraft designed for International Space Station (ISS) resupply missions. Initially developed by Orbital Sciences Corporation with financial support from NASA under the Commercial Orbital Transportation Services (COTS) program. To create Cygnus, Orbital paired a pressurized cargo module, largely based on the Multi-Purpose Logistics Module, built by Thales Alenia Space and previously used by the Space Shuttle for ISS resupply, with a service module based on Orbital's GEOStar, a satellite bus. After a successful demonstration flight in 2013, Orbital was chosen to receive a Commercial Resupply Services (CRS) contract. A larger Enhanced Cygnus was introduced in 2015. Orbital Sciences was renamed Orbital ATK in 2015 and Northrop Grumman purchased Orbital in 2018 and has continued to operate Cygnus missions. A further enlarged Mission B Cygnus is expected to be introduced in 2025.
Air-launch-to-orbit (ALTO) is the method of launching smaller rockets at altitude from a heavier conventional horizontal-takeoff aircraft, to carry satellites to low Earth orbit. It is a follow-on development of air launches of experimental aircraft that began in the late 1940s. This method, when employed for orbital payload insertion, presents significant advantages over conventional vertical rocket launches, particularly because of the reduced mass, thrust, cost of the rocket, geographical factors, and natural disasters.
Minotaur IV, also known as Peacekeeper SLV and OSP-2 PK is an active expendable launch system derived from the LGM-118 Peacekeeper ICBM. It is operated by Northrop Grumman Space Systems, and made its maiden flight on 22 April 2010, carrying the HTV-2a Hypersonic Test Vehicle. The first orbital launch occurred on 26 September 2010 with the SBSS satellite for the United States Air Force.
Stargazer is a Lockheed L-1011 TriStar built in 1974, that was modified in 1994 for use by Orbital Sciences as a mother ship for the Pegasus, a small-lift launch vehicle. As of October 2022, 45 rockets have been launched from Stargazer. Stargazer is the only L-1011 airframe still airworthy.
A space tug is a type of spacecraft used to transfer spaceborne cargo from one orbit to another orbit with different energy characteristics. The term can include expendable upper stages or spacecraft that are not necessarily a part of their launch vehicle. However, it can also refer to a spacecraft that transports payload already in space to another location in outer space, such as in the Space Transportation System concept. An example would be moving a spacecraft from a low Earth orbit (LEO) to a higher-energy orbit like a geostationary transfer orbit, a lunar transfer, or an escape trajectory.
Ionospheric Connection Explorer (ICON) is a satellite designed to investigate changes in the ionosphere of Earth, the dynamic region high in the atmosphere where terrestrial weather from below meets space weather from above. ICON studies the interaction between Earth's weather systems and space weather driven by the Sun, and how this interaction drives turbulence in the upper atmosphere. It is hoped that a better understanding of this dynamic will mitigate its effects on communications, GPS signals, and technology in general. It is part of NASA's Explorer program and is operated by University of California, Berkeley's Space Sciences Laboratory.
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The Scaled Composites Model 351 Stratolaunch or Roc is an aircraft built by Scaled Composites for Stratolaunch Systems to carry air-launch-to-orbit (ALTO) rockets, and subsequently repurposed to offer air launch hypersonic flight testing after a change of ownership. It was announced in December 2011, rolled out in May 2017, and flew for the first time on April 13, 2019, shortly after the death of founder Paul Allen. The aircraft features a twin-fuselage design and the longest wingspan ever flown, at 385 feet (117 m), surpassing the Hughes H-4 Hercules "Spruce Goose" flying boat of 321 feet (98 m). The Stratolaunch is intended to carry a 550,000-pound (250 t) payload and has a 1,300,000-pound (590 t) maximum takeoff weight.
Pegasus II, also known as Thunderbolt, was an air-launched orbital rocket under development in 2012–2015 by Orbital Sciences Corporation for use by Stratolaunch Systems.
The DARPA XS-1 was an experimental spaceplane/booster with the planned capability to deliver small satellites into orbit for the U.S. Military. It was reported to be designed to be reusable as frequently as once a day, with a stated goal of doing so for 10 days straight. The XS-1 was intended to directly replace the first stage of a multistage rocket by taking off vertically and flying to hypersonic speed and high suborbital altitude, enabling one or more expendable upper stages to separate and deploy a payload into low Earth orbit. The XS-1 would then return to Earth, where it could ostensibly be serviced fast enough to repeat the process at least once every 24 hours.
Orbital ATK Inc. was an American aerospace manufacturer and defense industry company. It was formed in February 9, 2015 from the merger of Orbital Sciences Corporation and parts of Alliant Techsystems (ATK). Orbital ATK designed, built, and delivered rocket engines, military vehicles, firearms, autocannons, missiles, ammunition, precision-guided munitions, satellites, missile approach warning systems, launch vehicles and spacecraft. The company was acquired by Northrop Grumman on June 6, 2018. The former Orbital ATK operations were renamed Northrop Grumman Innovation Systems and operated as a division until January 1, 2020 when a reorganization merged the operations into the company's other divisions.
NG-10, previously known as OA-10E, is the eleventh flight of the Northrop Grumman uncrewed resupply spacecraft Cygnus and its tenth flight to the International Space Station under the Commercial Resupply Services (CRS-1) contract with NASA. The mission launched on 17 November 2018, at 09:01:31 UTC. This particular mission is part of an extension of the initial CRS contract that enables NASA to cover the ISS resupply needs until the Commercial Resupply Services-2 (CRS-2) contract enters in effect.