NASA $23.8 B Moon Rocket in Big Trouble, SpaceX’s new Starship Solution 100x BETTER...

Every time a crewed starship lands on the moon, NASA could end up spending more than $4 billion. It sounds unrelated, but it's true. Because to bring those astronauts back to Earth, we still have to rely on SLS and Orion, two vehicles infamous for their enormous costs and repeated serious technical issues. And that's the bottleneck. But SpaceX isn't willing to accept that. They have a plan to remove NASA's hardware from the equation entirely using nothing but starship. Not just to save a ton of money, but to make the entire mission simpler than anyone thinks. So how exactly are they going to pull that off? Let's find out in today's episode of Alpha Tech. Right now, it's not just Elon Musk thinking long-term. NASA is looking at the same future. Both sides are aiming for a sustainable lunar base often called Moonbase Alpha. And this isn't about planting flags. It's about building infrastructure. We're talking about a fission surface power system, a compact nuclear reactor that can deliver steady power through the brutal two-week lunar night when solar simply isn't enough. We're talking about mass drivers, electromagnetic launch systems that could fire AI satellites or refined lunar materials into orbit at incredibly low cost, taking advantage of the moon's low gravity and vacuum. That's how you build a real space economy, ISRU, manufacturing on the surface, a permanent presence, and eventually a launch point for Mars. But none of this matters unless Starship HLS proves it can safely land on the moon and bring astronauts back to lunar orbit. That's the key step. Without it, there's no reusable high-cadence lunar system. Starship has always been pitched as a high-performance, low-cost vehicle built around reusability. Musk has suggested a standard Starship flight could eventually drop below $10 million. An HLS mission could run closer to $100 million, mainly because that version doesn't return to Earth. But that's not a deal-breaker. HLS can stay in lunar space and potentially become part of the base itself. Super Heavy still returns to the launch site and flies again. The real problem is this. Even if Starship HLS successfully lands astronauts on the lunar surface and brings them safely back to lunar orbit, the round trip between Earth and the moon still depends entirely on NASA's legacy architecture, Space Launch System, and Orion. And that's the bottleneck. These systems are often criticized as outdated because they inherit design philosophy and hardware lineage from Apollo and Constellation-era technology. They are not reusable. Their production chains are complex, and the cost reflects that reality. Each SLS launch is estimated at roughly $2 to $4 billion, not including Orion. The technical fragility only adds to the problem. On February 19th, NASA completed a second wet-dress rehearsal for Artemis to a full propellant loading test. On paper, that was progress. But shortly afterward, engineers detected a serious helium flow disruption in the interim cryogenic propulsion stage. The issue forced a rollback of the entire stack to the Vehicle Assembly Building for inspection and repair, eliminating the March 2026 launch window and pushing the mission at least into April, possibly later. This pattern is what turns Artemis into a slow, extremely expensive program vulnerable to recurring technical delays. It stands in direct contrast to the Starship philosophy, rapid reuse, low marginal cost per flight, and high launch cadence. Now consider the long-term vision. Building something like Moonbase Alpha won't take two astronauts. It could require 20 or more over multiple missions. Under the current SLS-Orion model, that could translate into $20 to $40 billion, largely funded by taxpayers. So the question becomes obvious. Why not remove SLS and Orion from the lunar transport chain altogether? If Earth-to-moon transport were handled entirely by Starship architecture, mission cost could drop by an order of magnitude. Instead of multi-billion dollar launches, the primary expenses would be propellant for Super Heavy and production of a Starship HLS variant potentially under $100 million per vehicle. Add crew salaries and operations, and you are no longer talking about billion-dollar missions. On paper, it makes economic sense. And this isn't just speculation. In late October 2025, after analyzing the data from Starship Flight 11, SpaceX appeared to uncover something significant. Whatever they saw in that data set clearly strengthened their confidence, confident enough that they formally proposed a simplified mission architecture to NASA, for Artemis 3, and the missions that follow. They haven't made the full details public. But based on what we know, the simplification likely points in one of two directions. Option one, remove SLS and Orion entirely. In other words, transport astronauts from Earth to the Moon and back using only Starship-based hardware. Option two, reduce the number of orbital refueling launches required to prepare HLS for lunar descent, streamlining the campaign and lowering operational complexity. Most analysts suspect the first option is the more radical and therefore the more intriguing. Because if SpaceX is truly proposing to cut SLS and Orion out of the loop, that would fundamentally reshape the Artemis architecture. So if that's the case, how would they actually pull it off? The sequence could start in a surprisingly straightforward way. NASA would still use Orion, fully assembled just like today. That means the crew capsule, the European service module, providing power propulsion, oxygen and water, and the launch abort system, the safety layer NASA insists on after the hard lessons of Challenger and Columbia. Altogether, that stack weighs somewhere in the 35 to 50 ton range. Here's the twist. Instead of sitting on top of SLS, Orion would ride inside Starship's payload bay. Starship would launch from LC-39A at Kennedy Space Center, or possibly from a new SpaceX pad. Raptor engines would push the entire stack to low Earth orbit roughly 200 kilometers up. Once stable in orbit, Starship would gently deploy Orion. Because this version of Starship would fly expendable, it could burn all remaining propellant to maximize Delta-V and push Orion as far as possible toward the moon before separation. From there, Orion takes over. Using the main engine on the European service module and possibly an additional kickstage if required, Orion would perform the translunar injection burn. Three to four days later, it reaches lunar space. No complex on-orbit assembly. No long chain of risky tanker refueling launches just to send crew beyond Earth orbit. Waiting near the moon would be Starship HLS, already fueled and staged in NRHO, or low lunar orbit. The four astronauts transfer from Orion to HLS, descend toward the lunar South Pole, perhaps near Shackleton Crater or other high-value scientific sites. They conduct EVAs, deploy instruments, collect samples, stay for several days, or even a couple of weeks. When the surface mission is complete, HLS lifts off, returns to lunar orbit, and docks again with Orion. The crew transfers back. HLS either remains in lunar space as infrastructure or follows whatever reuse plan SpaceX ultimately adopts. Orion then performs the return burn, accelerates toward Earth, reenters at high velocity using its proven heat shield, and splashes down in the ocean. No SLS. That single change could eliminate two to three billion dollars per mission, avoid the recurring hydrogen leak delays, and dramatically increase launch flexibility. At the same time, it would validate Starship as the true heavy lifter in the architecture. So, what do you think? Does it look cheaper and simpler? If you're still not convinced, then let's take a look at a second approach. One that doesn't need SLS and doesn't need Orion either. The concept leans fully into Starship as a unified, fully reusable system refined through recent test flights where orbital refueling has started to show real progress. The sequence begins in low Earth orbit, but instead of launching a single HLS vehicle, SpaceX would launch two Starships. First comes Starship HLS, the lunar-optimized lander version equipped with reinforced landing legs and a habitat capable of supporting astronauts on the surface for days or even weeks. It would launch from Starbase or LC-39A, reach LEO, and dock with a propellant depot for orbital refueling. Once fully fueled, HLS would perform a burn toward lunar orbit, staging itself either in near-rectilinear halo orbit or low lunar orbit depending on mission design and energy margins and wait there for the crew. Next comes the crew. Four astronauts, potentially more in future missions, would launch aboard a second Starship configured for crew transport. Unlike the pure HLS variant, this vehicle would be equipped with a heat shield for Earth reentry. It would launch to LEO dock with the depot refuel in orbit, and once topped off, execute the translunar injection burn. Three to five days later, it reaches lunar orbit. Compared to Orion, the crew would have significantly more volume and internal space during transit. No intermediate spacecraft. No separate capsule transfer. The crewed Starship would dock directly with the waiting HLS. From there, the mission shifts to the surface phase. The astronauts transfer into HLS and perform a propulsive descent to the lunar south pole. On the surface, they could deploy scientific instruments, test ISRU, hardware, operate rovers designed to explore or even mine water ice and conduct extended EVAs. Surface stays could last several days, possibly one to two weeks even longer, as early base modules are added. Compared to Apollo, this represents a major leap in endurance supported by advanced life support and the ability to deliver massive cargo capacity. When the surface mission is complete, HLS lifts off using its Raptor engines, taking advantage of lunar gravity at one-sixth of Earth's. No separate ascent stage required. It returns to lunar orbit and docks once again. For the return to Earth, the crew transfers back into the heat shield-equipped Starship. That vehicle performs trans-Earth injection and heads home. Upon arrival, it re-enters using its ceramic heat shield and aerodynamic flaps, followed by a propulsive landing either at sea or on land. No Orion required. Starship was designed from the beginning for high-energy re-entry and has undergone multiple test campaigns since 2024 to validate that capability. Economically, the difference is dramatic. A fully reusable Starship-based mission could potentially cost a few hundred million dollars compared to roughly four billion for a single SLS Orion flight. Just as important cadence increases, instead of waiting years between missions, launches could happen annually or even more frequently. It's a model aligned far more closely with Elon Musk's long-term vision, So, what do you think about this second approach? Compared to the first one, which direction makes more sense? Let me know in the comments. There's also a third option, and honestly, it might be the simplest and most practical of them all. Instead of using SLS and Orion-NASA, could use Crew Dragon launched on Falcon Heavy as the taxi to low-Earth orbit. The logic is straightforward. First, SpaceX launches Starship HLS and positions it in lunar orbit fully fueled and ready. Only after everything checks out does the crew launch aboard Crew Dragon, a system that has already flown dozens of operational missions to the ISS and proven itself highly reliable. The astronauts reach low-Earth orbit transfer to a waiting Starship configured for deep space and then head to the moon. They dock with HLS, descend to the surface, complete their mission return to orbit and eventually make their way back to Earth. In simple terms, you replace a multi-billion dollar launch system with one that costs tens of millions. This hybrid approach maximizes what already works. Falcon Heavy and Crew Dragon handle crew transport to orbit at relatively low cost. Starship handles the heavy lifting deep space transit and lunar landing. The result? No SLS, no Orion, dramatically lower cost, faster cadence and arguably higher operational flexibility.