The Star 48 is the largest of a family of solid rocket motors used by many space propulsion and launch vehicle stages, almost exclusively as an upper stage. It was developed primarily by Thiokol Propulsion and after several mergers, is manufactured by Northrop Grumman’s Space Systems division. A Star 48B stage is also one of the few man-made items sent on escape trajectories out of the Solar System, although it is derelict since its use. The Star 48B variant was the PAM-D upper stage used on the retired Delta II rocket.
 Star-48B rocket motor | |
| Country of origin | United States |
|---|---|
| Date | 1982–present |
| Manufacturer | Thiokol |
| Predecessor | Star 37 |
| Solid-fuel motor | |
The Star 48 has been used as an upper stage in three- and four-stage launch systems.
Overview
editThe "48" designation refers to the approximate diameter of the fuel casing in inches (122 cm); Thiokol had also manufactured other motors such as the Star 37 and Star 30. Internally, Thiokol's designation was TE-M-711 for early versions and TE-M-799 for later ones. Subtypes are given one or more letter suffixes after the diameter number, or a trailing number (i.e., "-2") after the internal designation. The "T" prefix stands for Thiokol, and the following letter refers to the company division that developed the rocket motor. In this case, "E" refers to the Elkton, MD division, and the "M" stands for the motor.
The Star 48 holds 2,000 kg of propellant. The most common use of the Star 48 was as the final stage of the Delta II launch vehicles. Other launchers such as ULA's Atlas 551 have also incorporated the motor but with lower frequency. On board the Space Shuttle, the complete stage (motor plus accessories) was referred to as the Payload Assist Module (PAM), as the Shuttle could only take satellites to low Earth orbit. Because geostationary orbit is much more lucrative, the additional stage was needed for the final leg of the journey. On such missions, the stage was spin-stabilized. A turntable, mounted in the shuttle payload bay or atop the previous Delta stage, spun the PAM and payload to approximately 60 rpm prior to release.
Usually after motor burnout and just prior to satellite release the PAM is de-spun using a yo-yo de-spin technique.
A Star 48 Payload Assist Module that had been used to launch a USA-91 GPS satellite in 1993 crashed in the Saudi Arabian desert in January 2001, after its orbit decayed. The unit did not burn up on reentry and was positively identified on the ground.[1]
A Star 48B motor used in the 3rd stage of the New Horizons probe was the first part of the New Horizons mission to reach Jupiter, arriving before the probe.[2] It also crossed Pluto's orbit in 2015 at a distance of 200 million kilometers.
In 2013 a Star 48GXV ("G" for "graphite case") was tested for the Solar Probe Plus mission (which later was renamed to the Parker Solar Probe)[3] but the development was cancelled, in favor of a Delta IV Heavy / Star 48BV combination.[4] for the launch in 2018.[5][6]
A non-spinning, thrust-vectoring version called Star 48BV is available, and is the final stage of the Minotaur IV+ launch vehicle.
Star 48B
editThe Star 48B version has an extra 11 kilograms of propellant more than the regular Star 48, for a total of 2011 kg.[7] There is a version of the Star 48B that is lengthened and also heavier, called the Star 48B L.[8]
In operation as a third stage, the Star 48B sits on top of the spin table, and before it is separated, it is spun up to stabilize it during the separation from the previous stage.[9] (see also spin-stabilisation) The Star 48B can produce 15,000 pounds of thrust (66723 newtons), with a burn time of 1 minute 27 seconds.[10]
Star 48B was used on the Atlas-E/F SGS-2,[11] and is the basis for the McDonnell Douglas PAM-D upper stage used on the Delta rocket.[10]
Use on New Horizons
editA Star 48B was used on the third stage of the New Horizons spacecraft launch.[12] New Horizons was launched by ULA's Atlas V 551 in January 2006, and the Star 48B booster was launched along with the New Horizons's spacecraft on an escape trajectory out of the Solar System.[13] The Star 48B ignited and burned for 48 seconds, taking both on a trajectory past Pluto; however, because the Star 48B became derelict and did not have course corrections like the NH spacecraft, it was projected to miss Pluto by hundreds of millions of miles.[13]
New Horizons' Star 48B was calculated to arrive at Jupiter six hours before New Horizons, and on October 15, 2015, passed through Pluto's orbit at a distance of 213 million kilometers (over 1 au) distant from Pluto.[13][14] This was nearly four months after the New Horizons probe did.[2]
Europa Clipper
editNASA intended to launch the Europa Clipper using a Star 48 on a SpaceX Falcon Heavy. The addition of a Star 48 "kick stage" would have allowed the Clipper mission to reach Europa without needing a gravity assist from Venus.[15] This was later removed with an updated Mars gravity assist route.[16]
Star 48 version details
edit| Name | Thiokol# | Mass (kg) | Prop. mass fract. | Imp. | Burn (s) | ||
|---|---|---|---|---|---|---|---|
| Total | Empty | Spec., Isp (s) | Tot. (kNs) | ||||
| Star 48 | TE-M-711-3 | 2114.0 | 114.2 | 0.946 | 286.6 | 5647.51 | |
| Star 48 | TE-M-711-8 | 2116.3 | 116.4 | 0.945 | 292.9 | 5766.23 | |
| Star 48A S | TE-M-799-1 | 2574.1 | 144.2 | 0.944 | 283.4 | 6798.70 | 87 |
| Star 48A L | TE-M-799 | 2582.3 | 152.4 | 0.941 | 289.9 | 6955.98 | 87 |
| Star 48B S | TE-M-711-17 | 2133.7 | 123.8 | 0.942 | 286.0 | 5674.77 | 84 |
| Star 48B L | TE-M-711-1 | 2140.5 | 130.6 | 0.939 | 292.1 | 5799.17 | 84 |
| Star 48BV | TE-M-940-1 | ||||||
See also
editReferences
edit- ^ "PAM-D Debris Falls in Saudi Arabia" (PDF). The Orbital Debris Quarterly News. 6 (2). NASA Johnson Space Center: 1. April 2001. Archived from the original (PDF) on 2004-07-28.
- ^ a b "Derelict Booster to Beat Pluto Probe to Jupiter". Space.com. 26 January 2006.
- ^ "ATK and NASA Successfully Demonstrate New Rocket Motor for Solar Probe Plus Mission". Prnewswire.com (Press release).
- ^ "Orbital ATK to Augment ULA Rocket for Launch of NASA Solar Probe". ExecutiveBiz. Retrieved 2017-02-12.
- ^ Clark, Stephen (March 18, 2015). "Delta 4-Heavy selected for the launch of solar probe". Spaceflight Now. Retrieved March 18, 2015.
- ^ "ULA's heavy-lifter rolled out for solar probe launch – Spaceflight Now". spaceflightnow.com. Retrieved 2018-11-05.
- ^ "Star 48B". Astronautix.com. Archived from the original on December 28, 2016. Retrieved 2018-10-22.
- ^ "Star 48B l". Astronautix.com. Archived from the original on December 28, 2016. Retrieved 2018-10-22.
- ^ Michael J. Muolo (1993). Space Handbook: A War Fighter's Guide to Space, V. 1. Government Printing Office. p. 126. ISBN 978-0-16-061355-5.
- ^ a b "PAM-D Payload Assist Module Archives - This Day in Aviation". This Day in Aviation. Retrieved 2018-10-22.
- ^ "Atlas-E/-F SGS-2 (Atlas-E/-F SVS-2)". Gunter's Space Page. Retrieved 2024-10-06.
- ^ "Press kit: NASA's First Mission to Pluto and the Kuiper Belt" (PDF). Nasa.gov. Retrieved 22 October 2018.
- ^ a b c Stern, Alan; Guo, Yanping (October 28, 2010). "Where Is the New Horizons Centaur Stage?". Johns Hopkins University Applied Physics Laboratory. Retrieved 2018-10-22.
- ^ "New Horizons trajectory: Star 48b Third-stage Motor". Unmannedspaceflight.com.
- ^ "SpaceX to launch the Europa Clipper mission for a bargain price". Arstechnica.com. 23 July 2021.
- ^ Brown, David. "EUROPA CLIPPER INCHES FORWARD, SHACKLED TO THE EARTH". SuperCluster. Retrieved 26 November 2022.
- ^ "Star-48". space.skyrocket.de. Retrieved 2024-10-06.