Science
Starlink Group 4-13 | Falcon 9 Block 5 – Everyday Astronaut


Featured image credit: SpaceX
Lift Off Time |
May 13, 2022 – 22:07 UTC | 15:07 PDT |
---|---|
Mission Name |
Starlink Group 4-13; the fifteenth launch to Starlink Shell 4 |
Launch Provider
|
SpaceX |
Customer
|
SpaceX |
Rocket |
Falcon 9 Block 5, B1063-5; 108.20 day turnaround |
Launch Location |
Space Launch Complex 4 East (SLC-4E), Vandenberg Space Force Base, California, USA |
Payload mass |
~16,250 kg (~35,800 lb) (53 x 307 kg, plus dispenser) |
Where did the satellites go? |
Starlink Shell 4; 540 km circular low-Earth orbit (LEO); initial orbit: 315 x 305 km at 53.22° |
Did they attempt to recover the first stage? |
Yes |
Where did the first stage land? |
B1063 successfully landed 642 km downrange on Of Course I Still Love You
Tug: Debra C; Support: GO Quest |
Did they attempt to recover the fairings? |
The fairing halves were recovered from the water ~654 km downrange by NRC Quest |
Were these fairings new? |
No, both fairing halves were flight proven |
This was the: |
– 153rd Falcon 9 launch – 93rd Falcon 9 flight with a flight proven booster – 97th re-flight of a booster – 18th re-flight of a booster in 2022 – 119th booster landing – 45th consecutive landing (a record) – 19th launch for SpaceX in 2022 – 23rd SpaceX launch from SLC-4E – 53rd orbital launch attempt of 2022 |
Where to watch |
Official Replay |
How Did It Go?
SpaceX’s Starlink Group 4-13 mission successfully launched 53 Starlink satellites atop a Falcon 9 rocket. The Falcon 9 lifted off from Space Launch Complex 4 East (SLC-4E), at the Vandenberg Space Force Base, in California, United States. Starlink Group 4-13 marked the 44th operational Starlink mission, boosting the total number of Starlink satellites launched to 2,547, of which 2,300 are in orbit around the Earth. Starlink Group 4-13 marked the 15th launch to the fourth Starlink shell; roughly 30 launches will be required to fill this shell.
What Is Starlink?
Starlink is SpaceX’s internet communication satellite constellation. The low-Earth orbit constellation will deliver fast, low-latency internet service to locations where ground-based internet is unreliable, unavailable, or expensive. The first phase of the constellation consists of five orbital shells.
Starlink is currently available in certain regions, allowing anyone in approved regions to order or preorder. After 28 launches SpaceX achieved near-global coverage, but the constellation will not be complete until ~42,000 satellites are in orbit. Once Starlink is complete, the venture is expected to profit $30-50 billion annually. This profit will largely finance SpaceX’s ambitious Starship program, as well as Mars Base Alpha.
A stack of 60 Starlink sattelites prior to be encapsulated into Falcon 9’s payload fairing. (Credit: SpaceX)
” data-medium-file=”https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-200×300.jpg” data-large-file=”https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-684×1024.jpg” width=”684″ height=”1024″ src=”https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-684×1024.jpg” alt=”Starlink satellites, satellite dispenser.” class=”wp-image-10398″ srcset=”https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-684×1024.jpg 684w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-200×300.jpg 200w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-768×1150.jpg 768w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-1026×1536.jpg 1026w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-1200×1797.jpg 1200w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-380×569.jpg 380w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-800×1198.jpg 800w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded-1160×1737.jpg 1160w, https://everydayastronaut.com/wp-content/uploads/2019/11/starlinksatsloaded.jpg 1282w” sizes=”(max-width: 684px) 100vw, 684px”>
What Is The Starlink Satellite?
Each Starlink V1.5 satellite has a compact design and a mass of 307 kg. SpaceX developed a flat-panel design, allowing them to fit as many satellites as possible into the Falcon 9’s 5.2 meter wide payload fairing. Due to this flat design, SpaceX is able to fit up to 60 Starlink satellites and the payload dispenser into the second stage, while still being able to recover the first stage. This is near the recoverable payload capacity of the Falcon 9 to LEO, around 16 tonnes.
As small as each Starlink satellite is, each one is packed with high-tech communication and cost-saving technology. Each Starlink satellite is equipped with four phased array antennas, for high bandwidth and low-latency communication, and two parabolic antennas. The satellites also include a star tracker, which provides the satellite with attitude data, ensuring precision in broadband communication.
Each Starlink V1.5 satellite is also equipped with an inter-satellite laser communication system. This allows each satellite to communicate directly with other satellites, not having to go through ground stations. This reduces the number of ground stations needed, allowing coverage of the entire Earth’s surface, including the poles.
The Starlink satellites are also equipped with an autonomous collision avoidance system, which utilizes the US Department of Defense (DOD) debris tracking database to autonomously avoid collisions with other spacecraft and space junk.
To decrease costs, each satellite has a single solar panel, which simplifies the manufacturing process. To further cut costs, Starlink’s propulsion system, an ion thruster, uses krypton as fuel, instead of xenon. While the specific impulse (ISP) of krypton is significantly lower than xenon’s, it is far cheaper, which further decreases the satellite’s manufacturing cost.
Ion Power
Each Starlink satellite is equipped with the first Hall-effect krypton-powered ion thruster. This thruster is used for both ensuring the correct orbital position, as well as for orbit raising and orbit lowering. At the end of the satellite’s life, this thruster is used to deorbit the satellite.
What Is The Starlink Satellite Constellation?
A satellite constellation is a group of satellites that work in conjunction for a common purpose. Currently, SpaceX plans to form a network of 11,716 satellites; however, in 2019 SpaceX filed an application with the Federal Communication Commission (FCC) for permission to launch and operate an additional 30,000 satellites as part of phase 2 of Starlink. To put this number of satellites into perspective, this is roughly 20 times more satellites than were launched before 2019.
Of the initial ~12,000 satellites, ~4,400 would operate on the Ku and Ka bands, with the other ~7,600 operating on the V-Band.
Due to the vast number of Starlink satellites, many astronomers are concerned about their effect on the night sky. However, SpaceX is working with the astronomy community and implementing changes to the satellites to make them harder to see from the ground and less obtrusive to the night sky. SpaceX has changed how the satellites raise their orbits and, starting on Starlink V1.0 L9, added a sunshade to reduce light reflectivity. These changes have already significantly decreased the effect of Starlink on the night sky.
Starlink Phase 1 Orbital Shells:
Inclination (°) | Orbital Altitude (km) | Number of Satellites | |
Shell 1 | 53.0 | 550 | 1,584 |
Shell 2 | 70.0 | 570 | 720 |
Shell 3 | 97.6 | 560 | 348 |
Shell 4 | 53.2 | 540 | 1,584 |
Shell 5 | 97.6 | 560 | 172 |
Shell 1
The first orbital shell of Starlink satellites consists of 1,584 satellites in a 53.0° 550 km low-Earth orbit. Shell 1 consists of 72 orbital planes, with 22 satellites in each plane. This shell is currently near complete, with occasional satellites being replaced. The first shell provides coverage between roughly 52° and -52° latitude (~80% of the Earth’s surface), and will not feature laser links until replacement satellites launch after 2021.
Shell 2
Starlink’s second shell will host 720 satellites in a 70° 570 km orbit. These satellites will significantly increase the coverage area, which will make the Starlink constellation cover around 94% of the globe. SpaceX will put 20 satellites in each of the 36 planes in the third shell. This shell is currently being filled, along with Shell 4.
Shell 3
Shell 3 will consist of 348 satellites in a 97.6° 560 km orbit. SpaceX deployed 10 laser link test satellites into this orbit on their Transporter-1 mission to test satellites in a polar orbit. SpaceX launched an additional three satellites to this shell on the Transporter-2 mission. On April 6, 2021, Gwynne Shotwell said that SpaceX will conduct regular polar Starlink launches in the summer, but this shell is now the lowest priority, and is expected to be the last filled. All satellites that will be deployed into this orbit will have inter-satellite laser link communication. Shell 4 will have six orbital planes with 58 satellites in each plane.
Shell 4
The fourth shell will consist of 1,584 satellites in a 540 km 53.2° LEO. This updated orbital configuration will slightly increase coverage area and will drastically increase the bandwidth of the constellation. This shell will also consist of 72 orbital planes with 22 satellites in each plane. This shell is currently being filled alongside Shell 2.
Shell 5
The final shell of Phase 1 of Starlink will host 172 satellites in another 97.6° 560 km low-Earth polar orbit. Shell 5 will also consist purely of satellites with laser communication links; however, unlike Shell 3, it will consist of four orbital planes with 43 satellites in each plane.
Starlink Phase 2 Orbital Shells:
Shell 6
The sixth orbital shell of Starlink satellites is permitted to consist of 2,493 satellites in a 42° 335.9 km LEO. This large number of satellites will decrease latency and increase bandwidth for lower latitudes.
Shell 7
The seventh Starlink shell permits SpaceX to deploy 2,478 satellites into a 48° 340.8 km low-Earth orbit. These satellites will further decrease latency and increase bandwidth for lower latitudes.
Shell 8
The final shell of Starlink Phase 2 allows SpaceX to deploy 2,547 satellites in a 53° 345.6 km orbit.
SpaceX has until March of 2024 to complete half of phase 1 and must fully complete Phase 1 by March of 2027. Phase 2 must be half complete by November of 2024, and be finished by November of 2027. Failure to do so could result in SpaceX losing its dedicated frequency band.
What Is Falcon 9 Block 5?
The Falcon 9 Block 5 is SpaceX’s partially reusable two-stage medium-lift launch vehicle. The vehicle consists of a reusable first stage, an expendable second stage, and, when in payload configuration, a pair of reusable fairing halves.
First Stage
The Falcon 9 first stage contains 9 Merlin 1D+ sea level engines. Each engine uses an open gas generator cycle and runs on RP-1 and liquid oxygen (LOx). Each engine produces 845 kN of thrust at sea level, with a specific impulse (ISP) of 285 seconds, and 934 kN in a vacuum with an ISP of 313 seconds. Due to the powerful nature of the engine, and the large amount of them, the Falcon 9 first stage is able to lose an engine right off the pad, or up to two later in flight, and be able to successfully place the payload into orbit.
The Merlin engines are ignited by triethylaluminum and triethylborane (TEA-TEB), which instantaneously burst into flames when mixed in the presence of oxygen. During static fire and launch the TEA-TEB is provided by the ground service equipment. However, as the Falcon 9 first stage is able to propulsively land, three of the Merlin engines (E1, E5, and E9) contain TEA-TEB canisters to relight for the boost back, reentry, and landing burns.
Second Stage
The Falcon 9 second stage is the only expendable part of the Falcon 9. It contains a singular MVacD engine that produces 992 kN of thrust and an ISP of 348 seconds. The second stage is capable of doing several burns, allowing the Falcon 9 to put payloads in several different orbits.
For missions with many burns and/or long coasts between burns, the second stage is able to be equipped with a mission extension package. When the second stage has this package it has a grey strip, which helps keep the RP-1 warm, an increased number of composite-overwrapped pressure vessels (COPVs) for pressurization control, and additional TEA-TEB.
Falcon 9 Booster
The booster that supported Starlink Group 4-13 is B1063. As the booster had supported 4 previous flights, its designation for Starlink Group 4-13 is B1063-5. This changed to B1063-6 upon successful landing.
B1063’s missions | Launch Date (UTC) | Turnaround Time (Days) |
Sentinel-6 | November 21, 2020 17:17 | N/A |
Starlink V1.0 L28 | May 26, 2021 18:59 | 186.07 |
DART | November 24, 2021 06:21 | 181.47 |
Starlink Group 4-11 | February 25, 2022 17:12 | 62.45 |
Starlink Group 4-13 | May 13, 2022 22:07 | 108.20 |
Following stage separation, the Falcon 9 conducted two burns. These burns softly touched down the booster on SpaceX’s autonomous spaceport drone ship Of Course I Still Love You.


Falcon 9 Fairings
The Falcon 9’s fairing consists of two dissimilar reusable halves. The first half (the half that faces away from the transport erector) is called the active half, and houses the pneumatics for the separation system. The other fairing half is called the passive half. As the name implies, this half plays a purely passive role in the fairing separation process, as it relies on the pneumatics from the active half.
Both fairing halves are equipped with cold gas thrusters and a parafoil which are used to softly touch down the fairing half in the ocean. SpaceX used to attempt to catch the fairing halves, however, at the end of 2020 this program was canceled due to safety risks and a low success rate. On Starlink Group 4-13, SpaceX recovered the fairing halves from the water with their recovery vessel NRC Quest.
In 2021, SpaceX started flying a new version of the Falcon 9 fairing. The new “upgraded” version has vents only at the top of each fairing half, by the gap between the halves, whereas the old version had vents placed spread equidistantly around the base of the fairing. Moving the vents decreases the chance of water getting into the fairing, making the chance of a successful scoop significantly higher.
An active Falcon 9 fairing half (Credit: Greg Scott)
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Falcon 9 Passive fairing half (Credit: Greg Scott)
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Half of the fairing being taken off Go. Navigator. (Credit: Lupi)
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Starlink Group 4-13 Countdown
All times are approximate
HR/MIN/SEC | EVENT |
---|---|
00:38:00 | SpaceX Launch Director verifies go for propellant load |
00:35:00 | RP-1 (rocket grade kerosene) loading underway |
00:35:00 | 1st stage LOX (liquid oxygen) loading underway |
00:16:00 | 2nd stage LOX loading underway |
00:07:00 | Falcon 9 begins engine chill prior to launch |
00:01:00 | Command flight computer to begin final prelaunch checks |
00:01:00 | Propellant tank pressurization to flight pressure begins |
00:00:45 | SpaceX Launch Director verifies go for launch |
00:00:03 | Engine controller commands engine ignition sequence to start |
00:00:00 | Falcon 9 liftoff |
Starlink Group 4-13 Launch, Landing, and Deployment
All times are approximate
HR/MIN/SEC | EVENT |
---|---|
00:01:12 | Max Q (moment of peak mechanical stress on the rocket) |
00:02:30 | 1st stage main engine cutoff (MECO) |
00:02:34 | 1st and 2nd stages separate |
00:02:40 | 2nd stage engine starts (SES-1) |
00:02:45 | Fairing deployment |
00:06:25 | 1st stage entry burn start |
00:06:44 | 1st stage entry burn complete |
00:08:10 | 1st stage landing burn start |
00:08:33 | 1st stage landing |
00:08:46 | 2nd stage engine cutoff (SECO-1) |
00:53:40 | 2nd stage engine starts (SES-2) |
00:53:41 | 2nd stage engine cutoff (SECO-2) |
01:02:42 | Starlink satellites deploy |
Science
Sea ice around Antarctica recedes to historically low levels: Scientists


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Science
Soyuz docks at International Space Station with two Russians, one American
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A Russian spacecraft carrying two Russians and an American docked at the International Space Station on Friday after blasting off from Kazakhstan.
NASA astronaut Loral O’Hara and Roscosmos cosmonauts Oleg Kononenko and Nikolai Chub departed from the Baikonur Cosmodrome in Kazakhstan and docked at the ISS approximately three hours later.
Per NASA, the trio will join the station’s Expedition 69 crew comprising astronauts from the U.S., Russia, Denmark, and Japan. O’Hara will spend six months there while Kononenko and Chub will spend a year.
The trio was supposed to fly to the space station earlier this year, but their original capsule, Soyuz MS-23, was needed as a replacement for another crew. That crew — also two Russians and an American — will ride it home on September 27. Their stay was extended from six months to a year when the capsule developed a coolant leak while parked at the station.
It’s the first spaceflight for O’Hara and Chub, while mission commander Kononenko is on his fifth trip to the orbiting outpost. By the end of his yearlong stay, Kononenko will set a new record for the longest time in space, more than a thousand days.
Original article source: Soyuz docks at International Space Station with two Russians, one American





Science
Exploring the effect of pain on response to reward loss in calves
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Abstract
Negative emotional states are known to interact, potentially aggravating one another. In this study, we used a well validated paradigm (successive negative contrast, SNC) to determine if pain from a common procedure (disbudding) influences responses to a reward downshift. Holstein calves (n = 30) were trained to approach a 0.5 L milk reward. Latency to approach, number of vocalisations and pressure applied on the bottle were recorded during training. To assess how pain affected responses to reward downshift, calves were randomly assigned to one of three treatments before the downshift. Two groups were disbudded and provided the ‘gold standard’ of pain mitigation: intraoperative local anesthesia and analgesia. One of these disbudded groups was then provided supplemental analgesic before testing. The third group was sham disbudded. All calves were then subjected to the reward downshift by reducing the milk reward to just 0.1 L. Interactions were detected between test session and daily trials on pressure applied for the Disbudded group (estimate ± SEM: 0.08 ± 0.05), and on vocalisations for the Sham (0.3 ± 0.1) and Disbudding + Analgesia (0.4 ± 0.1) groups. Our results indicate that SNC is a promising paradigm for measuring negative affect in calves and suggests that pain potentially affects the response to a reward downshift.
Introduction
A large body of research, primarily on rodents, has shown that sudden declines in reward levels are highly salient and provoke a negative affective response consistent with feelings of frustration or disappointment1,2. A well-developed paradigm for provoking this response is the successive negative contrast (SNC) test, where animals learn to obtain feed rewards which are then reduced in quantity or quality. Multiple lines of evidence indicate that this experience is distressing for animals, including increased levels of physiological markers of stress in rats and pigs3,4,5, and development of a preference for anxiolytic medication in rats6. In addition, responses to SNC are aggravated when an animal is in a pre-existing negative emotional state at the time of the test. For example, rats bred to be more anxious had higher latencies to approach a reward after a downshift7, and rats in amphetamine withdrawal displayed greater and longer reductions in reward consumption following a downshift8.
The influence of current affective state on SNC responses provides a compelling opportunity for the assessment of animal welfare, although only a handful of studies have employed this approach. In one study, rats housed in barren environments showed an extended increase in latency to approach the downshifted reward in comparison to rats housed in enriched environments, suggesting that these animals were more sensitive to reward loss than were rats in enriched housing9. Housing conditions (barren vs. enriched) also affected pigs’ sensitivity to reward loss10. To our knowledge, SNC has not been used to assess the emotional impact of pain in any species.
Research conducted on humans report that patients in a negative emotional state are more inclined to show anger responses11,12, and that pain can aggravate frustrating situations13.
In this study we tested if pain aggravates responses to SNC testing. Young cattle experience pain associated with routine farm procedures including hot-iron disbudding, indicated by physiological, behavioral and emotional responses to the procedure14,15,16,17,18. In this study we assessed the responses to SNC (in this case reducing the amount of milk available) in calves for three days following disbudding. Although providing a combination of local anesthesia and analgesia is considered a gold-standard in pain mitigation following disbudding, the duration of pain control has been challenging to estimate18, and disbudding pain has been suggested to last for several days19,20,21. For ethical reasons, all disbudded calves were provided local anesthesia and analgesia at the time of the procedure. To explore the potential longer-term pain caused by disbudding, a group of calves were provided additional fast-acting analgesia before tests. We predicted that calves in pain would respond to the downshift by increased pressure applied on the bottle containing the milk, number of vocalisations and latency to approach the reward. By exploring a novel approach to assessing the affective component of pain in animals, we hope to further the understanding of the emotional impact of a common farm procedure and, more generally, how negative states can interact to influence animal welfare.
Results
Maximum pressure applied to the reward bottle decreased across test days (− 0.4, t = − 3.5, P = 0.005) and daily trials (− 0.3, t = − 2.6, P = 0.01) (Fig. 1A). We also noted an interaction between test day and daily trial for the Disbudded group (0.1, t = 2.0, P = 0.05), and a tendency for the Sham group (0.08, t = 1.7, P = 0.09). There was no evidence of an interaction for pressure in the Disbudding + Analgesia group (0.07, t = 1.4, P = 0.2). Calves produced fewer vocalisations across days (− 1.5, t = − 4.6, P < 0.001) and daily trials (− 0.8, t = − 3.6, P < 0.001) (Fig. 1B). However, there were positive interactions between test day and trials for the Sham and Disbudding + Analgesia groups (0.3, t = 2.0, P = 0.05; 0.4, t = 2.7, P < 0.001 respectively). No interaction was found for the Disbudding group (0.05, t = 0.3, P = 0.7). Calves took longer to approach the reward across daily trials (0.4, t = 3.1, P = 0.002), with no effect of the test day (0.12, t = 0.9, P = 0.4) (Fig. 1C). Calves from the Sham group tended to decrease their latency across test day and daily trial (− 0.11, t = − 1.7, P = 0.09), whereas no interaction was found for the Disbudding (− 0.02, t = − 0.3, P = 0.8) and Disbudding + Analgesia groups (− 0.06, t = − 0.9, P = 0.3).
Calf responses to a reward downshift (from 0.5 L of milk to 0.1 L) over 3 test days, with 3 trials each day. An algometer was mounted behind the bottle containing the reward, measuring the maximum pressure exerted on the bottle by the calf (A). Vocalisations (B) and latency to approach (C) were also recorded. 24 h before the first test, calves were disbudded (Disbudding, Disbudding + Analgesia) or received a sham disbudding (Sham). One hour prior to tests, calves from the Disbudding + Analgesia group were administered an additional fast acting NSAID. Values presented are back transformed predicted values from mixed models. Colored circles represent mean estimates.
Discussion
After the reward downshift, calves responded by high pressure applied to the bottle and vocalisations. As calves went through more test sessions (with the lower reward), vocalisations and pressure both decreased, suggesting calves updated their expectations over time. Following the downshift, calves also increased their approach latency across trials within daily test sessions. This result is consistent with previous reports noting that approach latency increased after reward downshift 9,22.
We found some indication of a treatment effect on responses to the downshift over test days and daily trials. The significant positive interaction in pressure applied on the bottle over days and trials for the Disbudding group suggests some level of maintained frustration over tests. Similarly, only calves who had not been disbudded tended to decrease their approach latency across trials whereas calves from the Disbudding and Disbudding + Analgesia groups maintained their latency increase. This result is consistent with results from Burman and colleagues9 who reported a more prolonged response to reward downshift (i.e. higher latency) from rats assumed to be in a more negative affective state. This result is also consistent with work on calves showing increased anticipatory behavior in response to a reward downshift for animals housed in a more barren environment23. We had expected that calves receiving supplemental ketoprofen before the daily test sessions would have responded similarly to the sham calves. That these animals appeared to have some similar responses to the other disbudded calves suggests that our ketoprofen treatment protocol might not have mitigated the pain associated with disbudding during tests. Ketoprofen has been noted as appropriate pain control for disbudding24,25,26,27, but conflicting results have also been reported28,29.
In a study on SNC in chickens, Davies and colleagues30 found a gradual increase in approach latency and an immediate response in consummatory behaviours. They noted the gradual increase to be consistent with Thorndike’s law of effect31, analogous to an extinction mechanism where a less valuable reward induces a less ‘enthusiastic’ response over time. The disparity with consummatory responses was suggested to relate to the different timeframes of the measures: anticipatory responses such as approach latency might require conditioned learning, and therefore change more slowly. However, consummatory responses such as pressure applied are immediate indicators of reward evaluation, and therefore do not require an adjustment delay.
Contrary to our predictions, calves from the Disbudding group did not vocalize more than the other treatment groups after the downshift. These results remain unclear to us, but the very low number of vocalisations past the first test day questions the sensitivity of calves vocalisations counts when used in SNC paradigms.
The high variability among calves in their response to the downshift could be associated to intrinsic individual differences. Individual differences in traits such as fearfulness have been linked to pessimistic responses to a judgment bias test32. Moreover, such pessimism was also linked to the anhedonic response (i.e. a decrease in interest in a consummatory reward) following hot-iron disbudding33. Calves’ individual differences could also be dependent on the severity of the sensitization of their head caused by the procedure34,35, causing increased pain when coming into contact with the bottle. Alternatively, sucking on the nipple (even without milk) may be positive for calves36 and may also provide pain relief in the hours after disbudding37.
Conclusion
Following a reduction in a milk reward, calves who experienced a painful procedure appeared to potentially display an extended response to the downshift. Although SNC seems a promising avenue, our results remain tentative and further development of the paradigm and its applications must be investigated to identify its relevance to animal welfare assessment.
Methods
Ethics statement
Procedures were approved by The University of British Columbia Animal Care Committee under application A21-0111 and conducted in accordance with guidelines form the Canadian Council of Animal Care38. Reporting followed ARRIVE guidelines.
Animals and housing
The study was conducted at The University of British Columbia’s Dairy Education and Research Centre. To our knowledge, no study has used a similar paradigm in calves. To establish a sample size estimate, we relied on welfare studies using analogous SNC paradigms but applied to other species: rats (six subject per treatment9) and pigs (sixteen subjects per treatment group10). Considering this range and our own practical limitations, we settled on a sample size of ten subjects per treatment group. Thirty-five Holstein calves (all females) were initially enrolled in the study. Five calves were removed from the trial: three fell ill (scours and fever), one showed an extreme stress response when moved outside of her home pen, and one was not feed-restricted before a test. The thirty remaining had an average (± SD) birth weight of 38.3 ± 4.1 kg and were enrolled at 39.9 ± 4.1 d of age.
As routine farm practice, calves from all three treatments were intermingled in indoor pens (4.9 × 7.3 m, bedded with sawdust, and each containing eight to ten calves). Calves were provided ad libitum access to water and hay (RIC; Insentec B.V., Netherlands), and time-restricted access to 12 L of whole milk through a nipple feeder (CF 1000 CS Combi; DeLaval Inc., Sweden). To avoid long delay during trials, small replicates (average number of subjects per replicate = 3.5) were conducted.
Apparatus
The experimental apparatus was located in the same barn as the calves’ home pen, approximately 10–30 m away. The apparatus was a 1.8 × 1.2 m start-box leading to a 3.6 × 2.4 m pen through a vertical gate (Fig. 2A). Directly across from the start-box was a bottle and rubber teat mounted on rails, with an algometer (FPX 25, Wagner, Greenwich, USA) installed behind the bottle allowing measures of the maximum pressure applied to the bottle (Fig. 2B).
Calves were brought to the start-box, the vertical gate was lifted, and calves could access a milk reward (0.5 L during training, 0.1 L during tests) in the test pen (A). The bottle containing the milk reward was mounted on rails with an algometer positioned behind the bottle to measure the maximum pressure applied by the calf (B). Illustrations by Ann Sanderson.
Training
The trial was divided in three phases over seven days: training (three days), treatment (one day) and testing (three days). During training, calves were feed-restricted overnight (from 22:00 h) to ensure a high motivation for milk rewards over repeated trials. At approximately 10:00 h calves were individually brought into the apparatus, with no set order, and then placed in the start-box. The vertical gate was lifted and calves could approach and drink a 0.5 L milk reward from the bottle (this amount was based on previous studies on motivation trade-offs studies in calves37,39). Latency to contact the bottle (with mouth or tongue), latency to finish the reward, number of vocalisations and maximum pressure applied to the bottle were recorded live. The calf was then brought back to the start-box, the bottle refilled, and two more trials were conducted (i.e., for a total of three trials/d). After these trials were completed, the calf was returned to her home pen with full access to her daily milk allowance of (12 L/d). Training took place over three consecutive days, for a total of nine training trials. During the first day of training (for all three trials), no cues were given to the calf for the first minute after opening the start-box gate. After one minute, auditory (calls/whistle) and tactile (finger suckling) cues were given from the experimenter from outside the test-pen to get the calf’s attention towards the bottle. If these cues had failed after an additional minute, the experimenter would go inside the test pen and lead the calf to the bottle.
During the second and third day of training, no cues were given. If the calf had not approached the bottle within two minutes, the trial was recorded as a no-approach (and a pressure of zero applied to the bottle). Once a calf had approached the bottle, she had three additional minutes to finish the reward.
Treatments
Calves were pseudo-randomly assigned to one of three treatments (Disbudding, Disbudding + Analgesia, or Sham; ten calves each). Treatment assignment was balanced for age and birthweight (Disbudding: 40.7 ± 4.3 d, 38.7 ± 3.9 kg; Disbudding + Analgesia: 39.2 ± 7.0 d, 38.0 ± 5.6 kg; Sham: 39.7 ± 6.0 d, 38.3 ± 2.4 kg). On treatment day, calves were not feed-restricted and went through their treatment in their group pen at approximately 10:00 h. Regardless of treatment, calves were weighted and administered a multimodal pain mitigation strategy of sedative, local anesthesia and analgesia. The sedative was used to facilitate following injections and disbudding (xylazine 0.2 mg/kg Subcutaneous, Rompun 20 mg/mL, Bayer, Leverkusen, Germany). After sedation was reached (recumbency and eye rotation, approximately 10 min), a local anesthetic was injected as a cornual nerve block to mitigate the acute pain of the procedure (5 mL per side, lidocaine 2%, epinephrine 1:100,000, Lido-2, Rafter8, Calgary, AB, Canada), an NSAID was provided to minimize inflammation (meloxicam 0.5 mg/kg Subcutaneous, Metacam 20 mg/mL, Boehringer Ingelheim, Burlington, ON, Canada), and the horn bud area was shaved with an electric trimmer. Ten minutes after lidocaine injection, a pinprick test was done on the horn buds to test for pain reflex. For calves in the Disbudding and Disbudding + Analgesia treatments, a pre-heated electric dehorner (X30, 1.3 cm tip, Rhinehart, Spencerville, IN, USA) was applied to both horn buds until a consistent dark ring formed around each bud (requiring approximately 10 to 15 s). Calves from the Sham group were treated identically but instead of being disbudded, only pressure on the horn buds was applied with the plastic handle of the dehorner. After the procedure was completed, calves were positioned in sternal recumbency and left to recover in the pen. As the magnitude and duration of NSAID effects following disbudding remain unclear 18, calves from the Disbudding + Analgesia group received an additional NSAID injection (ketoprofen, 3 mg/kg, Subcutaneous, Anafen, 100 mg/mL, Boehringer Ingelheim, Ontario, Canada) 1 h before each of the three test sessions to provide supplemental pain control at the time of testing. Based on a previous study on the efficacy of ketoprofen after disbudding29, we expected ketoprofen to provide analgesic effects for up to 2 h following treatment.
Tests
In the three days following treatment, calves were tested for sensitivity to reward loss. Tests were similar to training: calves were brought individually to the apparatus after overnight feed restriction, and allowed access to a milk reward three times in a row (for a total of nine trials), but during testing the reward was reduced to 0.1 L. The time allowed for calves to approach and drink the reward was matched with their performance during training. Maximum pressure applied to the bottle, number of vocalisations and latency to approach were recorded. Calves from the Disbudding + Analgesia group received an additional NSAID injection (ketoprofen, 3 mg/kg, Subcutaneous, Anafen, 100 mg/mL, Boehringer Ingelheim, Ontario, Canada) 1 h before each of the three test sessions. After each session calves were returned to their home pen and again provided access to their full milk allowance (12 L). After the three test days calves were returned to routine farm care.
Statistical analysis
A mixed model was conducted on each outcome (maximum pressure, vocalisations and approach latency) on test phases (post treatment) using R’s lme4 package40. For pressure and latency, data were log transformed to fit model assumptions of linearity, normality and homoscedasticity. For vocalisation counts, we used a Poisson mixed model. Fixed factors were treatment (2 df), test day (1 df), daily trial (1 df) and their interaction (3 df). Daily trial, nested within day and Calf ID, was included as a random factor. Significance and tendency thresholds were set at P ≤ 0.05 and P ≤ 0.10, respectively. Data (Supplementary Information 1) and R code (Supplementary Information 2) are available in supplementary materials.
Data availability
The dataset and R code are freely available in supplementary materials.
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Acknowledgements
We thank the staff and students at The UBC Dairy Education and Research Centre for their help and support. We are especially grateful for the help provided by (alphabetical order) Joseph Lee, Kathen Lee, Emeline Nogues, Zimbabwe Osorio, Yasamin (Yas) Ranjbar, Russell Tucker, Raphaela Woodroffe and Emily Yau. This research was funded by a Discovery Grant (RGPIN-2016-0462) awarded to DMW from the National Sciences and Engineering Research Council of Canada.
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The authors declare no competing interests.
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Cite this article
Ede, T., von Keyserlingk, M.A.G. & Weary, D.M. Exploring the effect of pain on response to reward loss in calves.
Sci Rep 13, 15403 (2023). https://doi.org/10.1038/s41598-023-42740-8
- Received: 05 December 2022
- Accepted: 14 September 2023
- Published: 16 September 2023
- DOI: https://doi.org/10.1038/s41598-023-42740-8





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