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Vector-R

From Quire, the open reference·Two stage Launch vehicle, 60 kg payload to LEO·3 min read
Vector-R
Vector-R
FunctionSmall satellite launch vehicle
ManufacturerVector Launch
Country of originUnited States
Cost per launch2–3 million USD
Size
Height12 m
Diameter1.2 m
Mass5,000 kg
Stages2/3
Capacity
Payload to LEO
Mass​60 kg [1]
Payload to SSO
Mass​​26 kg [2]
Associated rockets
FamilyVector (rocket family)
Derivative workVector-H
ComparableElectron, Falcon 1, Firefly Alpha
Launch history
StatusActive
Launch sitesMojave Air and Space Port
Spaceport Camden
Pacific Spaceport Complex – Alaska (planned)
MARS Pad OB (planned)
Spaceport Florida Launch Complex 46 (planned)
Total launches2
Success(es)2
Failure0
First stage
Diameter​1.2 m (3 ft 11 in)
Powered by3 X Hadley
Maximum thrust15,000 lbf (67,000 N)
PropellantKerosene / LOX
Second stage
Diameter​​.635 m (2 ft 1.0 in)
Powered by​1 X LP-2
Maximum thrust​1,000 lbf (4,400 N)
Burn time433 seconds
Propellant​Propylene / LOX

Vector-R (Vector Rapid) is a two-stage orbital expendable launch vehicle under development by the American aerospace company Vector Launch to cover the commercial small satellite launch segment (CubeSats).[3] Vector Launch went bankrupt in December 2019 and re-emerged in October 2020.[4] Two prototypes were launched in 2017.

The rocket completed a maiden test flight at low altitude in May 2017.[5] Vector Launch was planning the maiden orbital launch from the Pacific Spaceport Complex in Alaska in 2019,[6] but paused operation in August 2019 due to an uncertain financing situation.[7]

An upgraded version of the Vector-R, called the Vector-H (Heavy), is in development as well.

Design#edit

Vector-R plans to use two stages with a 1.2-meter (3.9 ft) diameter first stage and 0.635-meter (2.08 ft) diameter second stage, both filled with propylene/LOX propellant. The main body of the rocket will be constructed using a lightweight carbon composite material.[8]

The launch vehicle's first stage was to be powered by three LP-1 LOX/propylene engines, delivering 81,000 newtons of force. The second stage was to be powered by one LP-2 LOX/propylene engine, delivering 4,400 newtons of force. The engines used a 3D-printed engine injector, designed with help from NASA's Science, Technology and Mission Directorate (STMD) Flight Opportunities program. This allows the injector to be produced as a single piece of hardware, instead of as individual components.[citation needed]

Vector was aiming the rocket at a launch cadence of 100 vehicles per year.[9]

Block 0.1#edit

The first two sub-orbital flight tests used the Vector-R Block 0.1 prototype model,[10] which was a full size aluminum air-frame of the Vector-R but with only one first stage engine.

Vector-RE1#edit

The Vector-RE1, a planned variant, was planned to use the same body as the standard Vector-R but include an electric powered third stage.[10]

Intended usage#edit

Vector-R was designed to launch a 60 kg (130 lb) payload to a 1,000 km (620 mi) Sun-synchronous orbit, suitable for CubeSats and other small satellites. The cost per launch was planned to be less than US$3 million, a price point that the company hoped would have allowed it to attract one hundred launches per year. Customers could have chosen to encapsulate their spacecraft in payload fairings provided by the company, which could be attached to the rocket shortly before launch, in several different configurations, such as fitting CubeSats dispensers or multiple satellites in a single fairing.

Vector used on-site payload integration for the early launches. However it was expected to be able to integrate payloads at their Arizona and California payload facilities and ship them to their launch sites.

Launch sites#edit

Mojave Spaceport
Mojave Spaceport Image: source and license

Vector-R launched from the Mojave Air and Space Port and Spaceport Camden for its flight tests. It had completed one test flight from each pad. Flight B0.002 was also the first launch from Spaceport Camden.

Vector planned to use the LC-46 launch site in Florida and the Mid-Atlantic Regional Spaceport (MARS) Pad 0B[11] for the Vector-R rocket, with the first all-up launches would have occurred from MARS Pad 0B.[12] Additionally, Vector investigated adding more minimal infrastructure launch pads either located on land in the US, or to launch the rocket from barges on the ocean.[2]

Vector had planned for the maiden orbital launch from Kodiak Spaceport Launch Complex earlier in 2019.[13]

Launch statistics#edit

Two low altitude suborbital test flights were performed in 2017.

Launch sites#edit

2017

2018

2019

Launch outcomes#edit

  •   Failure
  •   Partial failure
  •   Success
  •   Scheduled

Launch history#edit

Flight №Date / time (UTC)Rocket
configuration
Launch sitePayloadPayload massOrbitCustomerLaunch
outcome
B0.0013 May 2017
19:00[14]
Vector-R (P-19H)Mojave[15]None—N/aSub-orbitalVector LaunchSuccess
Flight test; maiden flight of the Vector-R; first engineering test, scaled down version; scheduled altitude 4,500 feet (1,400 m).
B0.002[16]2 August 2017
16:15
Vector-RCamden[17]Two customer payloads.Sub-orbitalAstro DigitalSuccess
Flight test; full prototype version, upgraded flight systems; the launch was delayed due to ignition detection failure; launch took place from a trailer; the peak altitude was about 5,000 ft (1,500 m).

Planned launches#edit

Due to the bankruptcy and subsequent re-emergence of Vector, These launches are uncertain.

Date / time (UTC)Rocket
configuration
Launch sitePayloadOrbitCustomer
TBAVector-RTBATBALEO?TBA
B1001;[18] First launch since re-emergence of bankruptcy.
TBAVector-RCamden[10]Sub-orbitalVector Launch
B0.003;[19] Flight-Test; Testing fairings, avionics, and thrust vector control
TBAVector-RPSCA[20]Unicorn 2A
Delfi-PQ 1[21]
LEOAlba Orbital
Delft University of Technology
First orbital and commercial flight of the Vector-R. PocketQube launch.
TBAVector-RMARS LP-0B / PSCALandmapper-HDLEOAstro Digital
Earth observation
TBAVector-ROpen Cosmos

See also#edit

References#edit

  1. ^ "Vector-R (Rapid)". Vector-launch.com. Archived from the original on 25 September 2018. Retrieved 27 October 2018.
  2. ^ a b "Vector-R : Payload User's Guide" (PDF). Vector-launch.com. Archived from the original (PDF) on 27 March 2018. Retrieved 27 October 2018.
  3. ^ "Vector Space Systems raises funds to develop small launch vehicle - SpaceNews.com". SpaceNews.com. 2016-04-26. Retrieved 2017-03-22.
  4. ^ "3. 2. 1. We're baaa-ack!".
  5. ^ "Vector has completed the first successful flight test of its new micro rocket". 2017-05-03. Retrieved 2017-05-04.
  6. ^ VECTOR (22 February 2018). "This week, Vector submitted its first launch application to the @FAANews to enable orbital launching from the Pacific Spaceport Complex - Alaska, later this year". @vectorspacesys. Retrieved 2018-02-25.
  7. ^ "Small satellite launcher Vector pauses operations after ousting CEO". 10 August 2019.
  8. ^ "Vector-R (Rapide) - Vector Space Systems". Vector Space Systems. Retrieved 2017-03-22.
  9. ^ "Tiny rocket company aims for 100 launches a year—and it just might succeed". Ars Technica. Retrieved 2017-03-22.
  10. ^ a b c "Vector". Space.skyrocket.de. Retrieved 27 October 2018.
  11. ^ "Vector to perform first orbital launches from Virginia". SpaceNews.com. 24 October 2017. Retrieved 27 October 2018.
  12. ^ Vector Space aims to expand launch ranges with minimal infrastructure pads NasaSpaceflight.com
  13. ^ VECTOR (22 February 2018). "This week, Vector submitted its first launch application to the @FAANews to enable orbital launching from the Pacific Spaceport Complex - Alaska, later this year". @vectorspacesys. Retrieved 2018-02-25.
  14. ^ "Vector Space Makes 1st Test Launch of Small-Satellite Rocket". Space.com. 3 May 2017. Retrieved 27 October 2018.
  15. ^ "Vector Becomes First to Complete Successful Flight Test of Launch Vehicle". PR Newswire. 3 May 2017. Retrieved 2017-11-11.
  16. ^ Vector. "Vector Successfully Launches First Ever Rocket from Spaceport Camden". www.prnewswire.com. Retrieved 27 October 2018.
  17. ^ Henning, Allyson (2 August 2017). "Camden Spaceport sees 1st launch". Jacksonville, FL: WJXT. Archived from the original on 2017-11-11. Retrieved 2017-11-11.
  18. ^ "11 Oct 22, Vector-R B1001. First mission soon". 11 October 2022. Retrieved 11 October 2022.
  19. ^ Cantrell, Jim (3 February 2018). "Our @vectorspacesys B0.003 vehicle being readied in our new factory in #Tucson for flight later in March testing multiple subsystems including fairings, avionics, and thrust vector control systems on a suborbital flight. Stay tuned !pic.twitter.com/54Nf3CwKiI". @jamesncantrell. Retrieved 2018-02-25.
  20. ^ "Vector planning first orbital launch this summer". SpaceNews.com. 20 February 2018. Retrieved 27 October 2018.
  21. ^ "Vector to Conduct Dedicated Launch of Alba Orbital PocketQube Satellites on First Orbital Attempt". PR Newswire. 8 March 2018. Retrieved 4 April 2018.

This article is mirrored from “Vector-R” on English Wikipedia, revision 1320693933, written by Wikipedia's contributors and licensed CC BY-SA 4.0. Editing it here creates a Quire copy with its own history.

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