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Clear out junk files and repair common Windows errorsFree Scan →Fix the driver behind crashes, sound loss and screen glitchesFind Drivers →There is no public, like-for-like payload-capacity winner between Falcon 9 and Vulcan. United Launch Alliance (ULA) publishes Vulcan payload figures for defined orbits and booster configurations; SpaceX’s May 9, 2025 Falcon Payload User’s Guide says Falcon 9 mass-to-orbit capabilities are available upon request. Falcon 9’s first stage is designed to survive atmospheric entry and be recovered. The reviewed Vulcan sources describe its configurations and missions but do not establish an operational stage-reuse system. For a launch decision, compare the target orbit, payload, trajectory, recovery profile, and mission services—not a single headline number.
What the comparison can—and cannot—tell you
Falcon 9 and Vulcan are launch vehicles used for different mission needs, and a useful comparison has to account for more than the rocket’s maximum advertised payload. The amount of mass a vehicle can place in orbit depends on the destination orbit and the specific mission configuration. Inclination, trajectory constraints, payload characteristics, and whether a stage is recovered all matter.
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The public performance information reviewed here is not symmetrical. ULA’s current Vulcan performance table gives payload capacities for multiple booster configurations and reference orbits. SpaceX’s May 9, 2025 Falcon Payload User’s Guide does not provide a public Falcon 9 mass-to-orbit table; it directs customers to request those capabilities. As a result, a figure from ULA’s table cannot be fairly set beside an assumed or unsourced Falcon 9 capacity and presented as a verified head-to-head result.
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That disclosure difference is not proof that one rocket can lift more than the other. It means the public figures available here do not support that conclusion. A customer comparing launch services would need performance data for the same target orbit and a defined mission profile from both providers.
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That distinction matters because “How much can it carry?” can mean several different things. A launcher may have one capacity for a low circular orbit, another for a more demanding inclination, and still another for a transfer orbit or direct delivery to a high-energy destination. The mission may also require a particular deployment sequence, payload envelope, or recovery profile. A single maximum number strips away these conditions and can make two unlike services look comparable when they are not.
Vulcan payload capacity depends on booster configuration and orbit
Vulcan is offered with zero, two, four, or six solid rocket boosters (SRBs). ULA’s current performance table, accessed in 2026, gives the following capacities for its LEO-Reference orbit:
| Vulcan configuration | ULA-listed capacity to LEO-Reference |
|---|---|
| Zero SRBs | 10,800 kg |
| Two SRBs | 19,000 kg |
| Four SRBs | 24,600 kg |
| Six SRBs | 27,200 kg |
ULA defines LEO-Reference as a 200 km circular orbit at 28.7 degrees inclination. These values apply to that specified reference condition and to the corresponding SRB configuration; they are not universal payload ratings for every orbit or mission. The largest listed figure, 27,200 kg, belongs to the six-SRB configuration in this reference orbit. The four-SRB configuration is listed at 24,600 kg to the same orbit.
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Changing the destination changes the comparison. ULA’s table also includes an ISS reference orbit of 407 km circular at 51.6 degrees, a polar reference orbit of 200 km circular at 90 degrees, and performance entries for medium Earth orbit (MEO), geostationary transfer orbit (GTO), geostationary orbit (GEO), and trans-lunar injection (TLI). Those are different destinations and trajectories; a mass figure for one should not be treated as the capacity for another. The reference altitudes and inclinations define orbit conditions, not additional payload capacities.
The table establishes that adding SRBs increases ULA’s listed LEO-Reference payload figure across the four configurations. It does not, by itself, establish which Vulcan configuration is right for a particular payload. That requires matching the mission’s target orbit and constraints to the vehicle’s available performance, rather than selecting the biggest number without context.
The configuration is part of the number. A 27,200 kg claim without the six-SRB and LEO-Reference qualifiers would omit the assumptions that make the figure meaningful. Likewise, the 24,600 kg rating is not the capacity of every Vulcan flight: it is ULA’s listed four-SRB performance to that defined reference orbit. The USSF-87 mission discussed below flew a four-SRB VC4S configuration, but its direct-to-GEO mission profile is not the LEO-Reference case in this table.
Orbit labels also need care. LEO is not one single orbit: altitude and inclination vary, and a polar orbit at 90 degrees is not the same reference condition as the 28.7-degree LEO-Reference orbit. The ISS reference is higher and has a different inclination again. GEO and GTO are also distinct: a transfer orbit is a route toward geostationary orbit, whereas GEO describes the destination orbit itself. TLI is an injection trajectory toward the Moon, not an Earth orbit. Comparing figures across these categories without their conditions can reverse the apparent result or misstate what a rocket can deliver.
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SpaceX’s May 9, 2025 Falcon Payload User’s Guide says mass-to-orbit capabilities for Falcon 9 and Falcon Heavy are available upon request. It does not give a public Falcon 9 mass capacity for the same defined orbits listed in ULA’s table. Therefore, this comparison does not assign Falcon 9 a number or rank the vehicles by payload mass.
A capacity figure only answers a useful question when its conditions are clear. The reader needs to know the destination orbit and inclination, the trajectory from the launch site, and the vehicle configuration and recovery profile. Payload volume and other mission constraints also matter: a payload must fit the launch service as well as meet the mass and orbital requirements. SpaceX’s guide lists several possible orbit services, but a public orbit list is not a substitute for a mission-specific mass value.
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For a genuine bid comparison, request provider performance for the same payload mass and volume, target orbit, inclination, and delivery conditions. Specify whether the mission calls for a particular injection profile or other service requirements. Without that matched information, comparing Vulcan’s published LEO-Reference value against an unattributed Falcon 9 number can create false precision.
In particular, do not treat an unsourced number repeated in a general rocket comparison as though it came from SpaceX’s current guide. The guide’s stated process is to request the relevant mass-to-orbit capability. A customer needs the answer for the selected mission, not a number detached from orbit, trajectory, and recovery assumptions. If the requested destination is an ISS-like orbit, polar orbit, GTO, or Earth-escape trajectory, those should be named in the request rather than summarized as simply “orbit.”
The disclosure difference is useful to understand, but it is not itself a performance verdict. ULA makes a detailed set of Vulcan reference values public; SpaceX directs readers to obtain Falcon mass performance on request. This allows readers to describe what each provider publishes, not infer that the more detailed public table proves a higher capacity or that the less public data indicate a lower one.
Reusability: Falcon 9’s first stage is designed for recovery
SpaceX describes Falcon 9’s first stage as designed to survive atmospheric entry and be recovered. Its guide says Block 5 changes included thermal-protection modifications intended to support rapid recovery and refurbishment. The guide also notes that recovering hardware allows it to be examined. This supports describing Falcon 9 as a reusable first-stage system.
That description applies to the first stage, not the complete rocket. The Falcon 9 upper stage is not described as reusable in the reviewed guide. Calling Falcon 9 simply “reusable” without saying which stage can be recovered can leave readers with the mistaken impression that the entire vehicle returns for another flight.
Recovery is also part of the mission comparison, not a separate score that can be added without qualification. A launch service’s payload performance must be evaluated for the mission profile being offered, including whether the first stage is recovered. The available public information here does not quantify a Falcon 9 payload difference between recovery profiles, so no numerical adjustment belongs in this comparison.
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1Clear out junk files and repair common Windows errors2Scan for outdated or missing drivers - takes under a minute3Repair Windows errors before they cause bigger problemsBlock 5’s thermal-protection modifications are tied in SpaceX’s guide to supporting rapid recovery and refurbishment; they do not mean the stage is ready to fly again without inspection or work. The guide’s note that recovered hardware can be examined is another important part of the picture. Recovery makes hardware available for examination and potential refurbishment, while the precise turn-around process and mission-specific performance are not quantified here.
It is therefore accurate to say that Falcon 9 is designed for first-stage recovery and that the design includes features intended to support reuse. It would go beyond these cited details to assign a specific per-flight cost saving, turnaround time, or payload penalty. No such figures are provided here, and none should be invented to make reusability look like a simple advantage measurable in one number.
What the available Vulcan material establishes about reuse
ULA’s Vulcan specification describes a booster powered by BE-4 engines, optional SRBs, and a Centaur V upper stage. The reviewed specification, certification release, and mission material describe the vehicle and its operations; they do not document an operational Vulcan stage-recovery and reuse system. Accordingly, the evidence here supports a narrow conclusion: Falcon 9’s first-stage recovery design is documented, while these Vulcan sources do not establish operational stage reuse.
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This distinction is important. Not finding operational reuse documented in these sources is not a claim about every concept or proposal associated with a vehicle. It is also not a basis for describing Vulcan as having a working reusable stage. For a practical comparison based on the information available here, count Falcon 9’s first-stage recovery design as established and do not assign Vulcan an operational reuse capability.
That wording keeps the comparison tied to what is documented rather than making a claim about what might be proposed or technically possible. It also avoids turning the comparison into an unsupported cost calculation. Stage recovery can be one factor in choosing a launch service, but no cost-per-launch, refurbishment expense, or fleet-economics figures are established here for either rocket. A reader should not assume that a reusable stage automatically makes a mission cheaper, or that the absence of documented operational reuse alone determines the best vehicle for a mission.
Mission types and destinations
Falcon 9: satellite, rideshare, crew, cargo, and escape trajectories
SpaceX’s guide lists Falcon 9 services to low Earth orbit (LEO), polar and sun-synchronous LEO, GTO, and Earth-escape trajectories. Available orbit options depend on launch site and mission constraints. The guide also describes deployment of multiple satellites and dedicated small-satellite rideshare service.
NASA describes Falcon 9 as the launch vehicle used for Commercial Crew missions to the International Space Station (ISS). NASA also describes the rocket’s earlier satellite-launch, cargo-delivery, and cargo-return roles. That breadth makes Falcon 9 relevant to missions beyond placing a single satellite in orbit: its documented service history and offerings include crew and cargo operations as well as commercial satellite launches.
These are different kinds of service, not interchangeable payload labels. A dedicated satellite launch, a deployment carrying multiple spacecraft, and a small-satellite rideshare all involve different manifest needs. Crew missions to the ISS and cargo-delivery or return operations are another category altogether. The fact that Falcon 9 has these roles is relevant when a mission needs crew or cargo capability; it does not establish that every Falcon 9 flight is configured for those services.
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The orbit menu also spans very different destinations. Polar and sun-synchronous LEO are useful to distinguish from a generic LEO label, while GTO and Earth-escape trajectories indicate destinations beyond an ordinary low orbit. SpaceX’s guide conditions orbit availability on launch site and mission constraints, so a listed service should be understood as an option to evaluate rather than a promise that every mission profile is available from every site.
Vulcan: multiple orbit classes and high-energy insertions
ULA’s performance table covers LEO-Reference, ISS orbit, polar LEO, MEO, GTO, GEO, and TLI. The specific payload values vary by the orbit and booster configuration; the table’s LEO-Reference numbers should not be transferred to these other destinations. ULA presents Centaur V as providing flexibility and endurance for complex orbital insertions.
A concrete example is USSF-87. On February 12, 2026, a four-SRB VC4S Vulcan flew the mission carrying a multi-manifest national-security payload directly to geosynchronous orbit. This illustrates a direct-to-GEO national-security mission; it does not establish that every payload or mission can use that same configuration or delivery profile.
ULA announced on March 26, 2025, that the U.S. Space Force had certified Vulcan for National Security Space Launch (NSSL) missions. That is a dated certification milestone. It should not be read as a guarantee that any mission can be exchanged between Vulcan and another provider without regard to orbit, payload, schedule, or mission-specific requirements.
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ULA president and CEO Tory Bruno described the Centaur V role in the certification release: “Vulcan’s Centaur upper stage is a high-velocity and maneuverable platform to address evolving on-orbit threats in this new space warfighting domain and will offer extreme on-orbit endurance and flexibility for complex orbital insertions to meet the changing landscape and requirements of our nation.” This is ULA’s executive describing its own vehicle, not an independent assessment. It helps explain the company’s emphasis on upper-stage endurance and insertion flexibility, but it should not be treated as a separate quantified performance rating.
The mission example is also a useful reminder that “Vulcan capability” can refer to a concrete flight configuration and destination, while the table provides standardized reference cases. USSF-87’s VC4S configuration and direct GEO delivery illustrate a specific national-security mission. They do not turn the 24,600 kg LEO-Reference rating into a GEO payload figure, and they do not show that all Vulcan flights use four SRBs.
Compare the rockets against the mission you actually need
For an engineering or procurement comparison, first write down the mission conditions. A “payload capacity” question that omits orbit and configuration is incomplete; a “reusability” question that does not identify the stage can be misleading. The following checklist separates the factors that need to be matched.
- Target orbit and inclination: Record the destination precisely, including altitude and inclination where applicable. LEO-Reference, an ISS-like orbit, polar LEO, GEO, and TLI are not interchangeable conditions.
- Launch site and trajectory: Identify launch-site and trajectory constraints. SpaceX notes that Falcon 9 orbit options depend on these and other mission constraints.
- Vehicle configuration: For Vulcan, specify zero, two, four, or six SRBs. Do not attribute a six-SRB performance value to the four-SRB configuration flown on USSF-87.
- Recovery profile: State whether the requested service includes first-stage recovery. Recovery is a Falcon 9 first-stage design feature, but the reviewed public guide does not provide a matched payload adjustment for recovery.
- Payload fit: Give payload mass and volume, along with any deployment or manifest needs. Mass alone does not show whether the payload fits the available service.
- Injection and mission services: Specify whether the mission requires direct insertion into a high-energy destination, multiple satellite deployment, small-satellite rideshare, crew transport, cargo delivery, or cargo return.
After those conditions are fixed, request or consult provider performance for that exact profile. The useful outcome is a mission-specific offer, not a generic winner. One vehicle may be suitable for a particular service while another may serve a different orbit or operational requirement; the facts here do not support ranking them across every case.
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A free scan shows the junk files, broken settings and background clutter dragging Windows down - then fixes them in one click.Free scan · Windows 10 & 11A careful request should be concrete enough that the answers can be compared side by side. State the destination orbit and inclination, the payload’s mass and volume, the desired delivery or injection conditions, and whether the mission is dedicated or part of a multi-payload deployment. Include any requirements for rideshare, crew, cargo delivery, or cargo return. For Vulcan, identify the SRB configuration under consideration; for Falcon 9, ask for the provider’s mass-to-orbit capability for the stated mission and recovery profile. This keeps the comparison focused on comparable service rather than advertised maxima.
There are also limits to what a public table can settle. A table of reference-orbit payload values is useful for understanding how ULA publishes performance, but a launch buyer still needs a mission-specific assessment. Conversely, a provider’s request-based disclosure does not mean the mission cannot be evaluated; it means readers should not substitute a generic online claim for the provider’s requested mission data. In either case, the same orbit and delivery assumptions are necessary for a sound comparison.
Independent reader supportYour contribution helps us test, update, and keep practical guides available for everyone.What to take away from the published figures
The defensible capacity statement is specific: ULA lists Vulcan at 10,800 kg with no SRBs, 19,000 kg with two, 24,600 kg with four, and 27,200 kg with six for its 200 km, 28.7-degree LEO-Reference orbit in a current table accessed in 2026. SpaceX’s May 2025 guide says Falcon mass-to-orbit capability is available upon request, so a public, matched Falcon 9 number is not established here.
On reuse, SpaceX documents Falcon 9 first-stage recovery design, including Block 5 thermal-protection changes for recovery and refurbishment. The reviewed Vulcan materials do not establish operational stage reuse. On mission types, Falcon 9’s documented roles include satellite and rideshare launches, crew and cargo missions, and listed Earth-escape service; Vulcan’s published orbit envelope includes LEO through TLI and a 2026 example of a direct-to-GEO national-security mission. The right comparison depends on which of those requirements the mission has.
So the short answer is conditional, not a tie-breaker based on one published maximum. Vulcan has a public configuration-by-orbit table, and its LEO-Reference payload figure rises with SRB count. Falcon 9’s comparable mass values are not in the cited public guide. Falcon 9 has a documented recoverable first stage, while the cited Vulcan materials do not establish operational stage recovery and reuse. Both vehicles serve more than one kind of mission, but their published examples and service descriptions differ. Match the orbit, configuration, and required service first; then compare the provider data for that exact job.
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Frequently Asked Questions
Which carries more payload, Falcon 9 or Vulcan?
There is no defensible public, like-for-like winner from the cited material. ULA publishes Vulcan capacities by configuration and reference orbit, while SpaceX’s May 9, 2025 guide says Falcon 9 mass-to-orbit capabilities are available upon request. Compare provider data for the same orbit, inclination, trajectory, and recovery profile.
What is Vulcan’s payload capacity to LEO?
ULA lists 10,800 kg with zero SRBs, 19,000 kg with two, 24,600 kg with four, and 27,200 kg with six to its LEO-Reference orbit: a 200 km circular orbit at 28.7 degrees inclination. These are not capacities for every LEO orbit or for other destinations.
Is Falcon 9 reusable?
SpaceX describes Falcon 9’s first stage as designed to survive atmospheric entry and be recovered. Its guide notes Block 5 thermal-protection changes intended to support recovery and refurbishment. The guide does not describe the upper stage as reusable, so it is most precise to call Falcon 9 a reusable first-stage system.
Is Vulcan reusable?
The cited ULA specification, certification release, and mission material do not establish an operational Vulcan stage-recovery and reuse system. That is a statement about what those materials document, not a claim about every concept or proposal.
What missions can Falcon 9 launch?
SpaceX’s guide lists LEO, polar and sun-synchronous LEO, GTO, and Earth-escape services, as well as multiple-satellite deployment and dedicated small-satellite rideshare. NASA describes Falcon 9’s roles in Commercial Crew missions to the ISS and earlier satellite, cargo-delivery, and cargo-return missions.
What orbits and missions does Vulcan support?
ULA’s table includes LEO-Reference, ISS orbit, polar LEO, MEO, GTO, GEO, and TLI. A dated example is USSF-87, flown on February 12, 2026, by a four-SRB VC4S Vulcan carrying a multi-manifest national-security payload directly to geosynchronous orbit.
Does Vulcan’s four-SRB LEO rating apply to USSF-87?
No. The 24,600 kg value is ULA’s rating for four-SRB Vulcan to the defined 200 km, 28.7-degree LEO-Reference orbit. USSF-87 also used a four-SRB VC4S, but flew a direct-to-GEO mission; the LEO-Reference rating is not a GEO payload figure.
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What should I compare when choosing a launch service?
Match the target orbit and inclination, launch site and trajectory constraints, vehicle configuration, recovery profile, payload mass and volume, and required injection or service. Also identify needs such as satellite deployment, rideshare, crew transport, cargo delivery, or cargo return. Ask each provider for performance under the same mission conditions.
The Bottom Line
Bottom line: ULA’s public Vulcan table shows how capacity changes with SRB configuration and orbit; SpaceX’s May 2025 guide directs customers to request Falcon 9 mass-to-orbit data. Falcon 9’s first stage is designed for recovery, while the cited Vulcan sources do not establish operational stage reuse. Compare matched mission profiles rather than treating one headline capacity as a universal winner.
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