Boeing Small Launch Vehicle
The Boeing Small Launch Vehicle, or SLV, is an air-launched three-stage-to-orbit launch vehicle concept aimed to launch small payloads of {{convert|100|lb|kg}} into low Earth orbit. The program is proposed to drive down launch costs for small satellites as low as {{currency|300000|USD}} per launch ($7,000/kg) and could be fielded by 2020.{{cite news |last=Norris |first=Guy |title=Boeing Unveils Air-Launched Space-Access Concept |url=http://www.aviationweek.com/Article.aspx?id=/article-xml/AW_05_21_2012_p25-458597.xml&p=1 |accessdate=2012-05-23 |newspaper=Aviation Week |date=2012-05-21 |archive-date=2013-03-26 |archive-url=https://web.archive.org/web/20130326232014/http://www.aviationweek.com/Article.aspx?id=%2Farticle-xml%2FAW_05_21_2012_p25-458597.xml&p=1 |url-status=dead }} {{Update inline|date=December 2021}}
History
In July 2012, DARPA awarded Boeing a US$4.5 million contract to further refine the system concept as a part of the DARPA ALASA program.
{{cite news |last=Messier|first=Doug |title=DARPA Awards 6 Small Airborne Launch Vehicle Contracts |url=http://www.parabolicarc.com/2012/07/02/darpa-awards-6-small-airborne-launch-vehicle-contracts/ |accessdate=2012-11-29 |newspaper=Parabolic Arc |date=2012-07-02 }}
Description
The first stage of the three-stage launcher would be an air-launched supersonic aircraft accelerating to a speed of {{convert|4.5|Mach}} at {{convert|61000|ft}}, while the second stage would be a hypersonic waverider aircraft which would accelerate the vehicle to {{convert|10|Mach}} at an altitude of {{convert|95000|ft}}. Both of the first two stages would be reusable to reduce launch cost, and both stages would carry only fuel, and obtain their oxygen for combustion from the Earth's atmosphere.
The third stage would be powered by a rocket, roughly {{convert|16|ft}} long, to complete the acceleration of the {{convert|21|x|38|in|cm}} payload to orbital velocity.
The carrier aircraft is projected to be a Scaled Composites White Knight Two.
===Specifications===
- First-stage: {{convert|38|ft}} length, {{convert|19|ft}} wingspan, supersonic aircraft{{cite news |title=More on Boeing's small launcher concept |url=http://www.aviationweek.com/Blogs.aspx?plckPostId=Blog:a68cb417-3364-4fbf-a9dd-4feda680ec9cPost:f6f267a4-b412-44cc-a2a0-5258308c847e |archive-url=https://archive.today/20130118044523/http://www.aviationweek.com/Blogs.aspx?plckPostId=Blog:a68cb417-3364-4fbf-a9dd-4feda680ec9cPost:f6f267a4-b412-44cc-a2a0-5258308c847e |url-status=dead |archive-date=18 January 2013 |accessdate=4 Aug 2012 |newspaper=Aviation Week |date=22 May 2012 }}
- Second-stage: {{convert|37|ft}} in length, {{convert|15.3|ft}} wingspan, hypersonic aircraft; "Overall airframe construction would be of graphite-epoxy, with an integral conformal liquid methane tank to supply the vehicle’s circular combustion scramjet. Thermal protection would be a ceramic matrix composite material."
- Third-stage: {{convert|2|ft}} diameter, {{convert|16.4|ft}} long, solid propellant rocket.
- Payload: {{convert|21|in|m}} diameter, {{convert|38|in|m}} long payload bay, carrying up to {{convert|100|lb}} to low Earth orbit.
See also
- X-51 WaveRider hypersonic test vehicle flown at {{convert|5.1|Mach|sigfig=2|60,000}} at {{convert|60000|ft}} on a single test mission in May 2013.
References
{{Reflist}}