Starship Users Guide

© Space Exploration Technologies Corp. All rights reserved. STARSHIP USERS GUIDE Revision 1.0 | March 2020 COPYRIGHT Subject to the existing rights of third parties, Space Exploration Technologies Corp. (SpaceX) is the owner of the copyright in this work, and no portion hereof is to be copied, reproduced, or disseminated without the prior written consent of SpaceX.

STARSHIP PAYLOAD GUIDE COMPANY DESCRIPTION SpaceX was founded in 2002 to revolutionize access to space and enable a multi-planetary society. Today, SpaceX performs routine missions to space with its Falcon 9 and Falcon Heavy launch vehicles for a diverse set of customers, including the National Aeronautics and Space Administration (NASA), the Department of Defense, international governments, and leading commercial companies. SpaceX provides further support to NASA with the Dragon spacecraft by conducting cargo resupply and return missions to and from the International Space Station (ISS). Soon, SpaceX will begin transporting crew to the ISS as well. To offer competitive launch and resupply services, SpaceX has incorporated reusability into the Falcon and Dragon systems, which improves vehicle reliability while reducing cost. The Starship Program now leverages SpaceX’s experience to introduce a next- generation, super heavy-lift space transportation system capable of rapid and reliable reuse. STARSHIP PROGRAM OVERVIEW SpaceX’s Starship system represents a fully reusable transportation system designed to service Earth orbit needs as well as missions to the Moon and Mars. This two-stage vehicle—composed of the Super Heavy rocket (booster) and Starship (spacecraft) as shown in Figure 1—is powered by sub-cooled methane and oxygen. Starship is designed to evolve rapidly to meet near term and future customer needs while maintaining the highest level of reliability. STARSHIP USERS GUIDE Starship has the capability to transport satellites, payloads, crew, and cargo to a variety of orbits and Earth, Lunar, or Martian landing sites. Potential Starship customers can use this guide as a resource for preliminary payload accommodations information. This is the initial release of the Starship Users Guide and it will be updated frequently in response to customer feedback. PAYLOAD CONFIGURATIONS Starship crew and uncrewed configurations are shown in Figure 2. The uncrewed Starship allows for the transport of satellites, large observatories, cargo, refueling tanks or other unmanned assets. Subsequent sections provide an overview of the preliminary volume and mechanical interfaces available; preliminary Figure 1: Starship and Super Heavy payload environments expected; and the preliminary mass-to-orbit capabilities of Starship. Please contact [email protected] to evaluate how Starship can meet your unique needs. © Space Exploration Technologies Corp. All rights reserved. 1

STARSHIP PAYLOAD GUIDE Figure 3: Starship payload deployment sequence PAYLOAD VOLUME Starship’s 8 m diameter payload dynamic envelope is shown in Figure 4. This large deployable envelope allows for the design of novel payloads, rideshare opportunities and entire constellations of satellites on a single launch. An extended payload volume is also Figure 2: Starship crew (left) and uncrewed (right) available for payloads requiring up to 22 m of height. configurations PAYLOAD MECHANICAL INTERFACES PAYLOAD FAIRING The standard Starship payload fairing is 9 m in outer diameter resulting in the largest usable payload volume of any current or in development launcher. The Starship payload fairing is a clamshell structure in which the payload is integrated. Once integrated, the clamshell fairing remains closed through launch up until the payload is ready to deploy. An example sequence of payload deployment is shown in Figure 3. To deploy the payload, the clamshell fairing door is opened, and the payload adapter and payload are tilted at an angle in preparation for separation. The payload is then separated using the mission-unique payload adapter. If there are multiple payloads on a single mission, a rotating mechanism can be provided to allow each satellite to separate with maximum clearance. Once separation is confirmed and the payload(s) have cleared the fairing, the payload fairing door is closed in preparation for Starship’s return to Earth. Figure 4: Starship payload volume (dimensions in m) © Space Exploration Technologies Corp. All rights reserved. 2

STARSHIP PAYLOAD GUIDE PAYLOAD MANIFESTING commanded after integration into the fairing without Satellite customers may be manifested on single or facility located payload EGSE. This covers final pre- multi-manifest missions. Customers can bring a single launch events in the processing facility and on the spacecraft, coordinate their own rideshares for a single launch pad, and some of these electrical interfaces Starship launch, or work with SpaceX to take may continue to be available in-flight. Contact advantage of a multi-manifest launch. Customer [email protected] for more information or other missions do not need to wait for co-passengers in order options. to fly. The unique and large geometry of the Starship payload ENVIRONMENTS bay also opens new opportunities for payload Utilizing strong heritage and lessons learned from the integration. For payloads requiring additional structural development of the Falcon 1, Falcon 9 and Falcon support, Starship has the ability to mount supports Heavy launch systems, SpaceX is designing Starship along the sidewalls or nose to interface with trunnion- and Super Heavy to provide as benign of a payload style interfaces on the payloads, similar to those environment as possible. SpaceX will ensure that employed on NASA’s Space Shuttle orbiters. When Starship environments meet or improve upon those of large payloads are co-manifested on Starship, they are the Falcon Heavy launch system. To aid in the design generally mounted side-by-side on the payload of space vehicles capable of flying on Starship, adapter. This reduces technical and schedule SpaceX is providing the following preliminary payload dependencies between rideshare participants environments. compared to stacked configurations. Example single-mission manifests: LOADS  1-3x geosynchronous telecom satellite(s) SpaceX is designing Starship to ensure that  Full constellation of satellites on a single acceleration environments are well within industry mission standard levels. During flight, the payload will experience a range of axial and lateral accelerations.  1-2x geosynchronous telecom satellites plus Both the Super Heavy and Starship engines can be rideshare system of small satellites throttled to help maintain launch vehicle and payload  In-space demonstration spacecraft that remains acceleration limits. integrated with Starship and returns to Earth  Cargo and crew configurations PAYLOAD ADAPTERS The Starship payload attach fitting is designed to accommodate standard payload interface systems in single- or multi-manifest configurations. SpaceX will either provide and integrate a payload adapter and clampband separation system or will integrate an adapter and separation system provided by the customer. As a baseline, Starship is compatible with heritage Falcon 937-mm, 1194-mm, 1666-mm and 2624-mm clampband interface requirements, including Figure 5: Payload maximum design load factors the ability to host multiple payloads side by side given the large diameter available. For customers with The maximum expected design load factors for a single alternative interface requirements, SpaceX has a wide payload mission launching on Starship are shown in breadth of experience designing and manufacturing Figure 5. Actual payload dynamic loads, accelerations, non-standard adapters and separation systems. and deflections are a function of the dynamic coupling between Starship and the payload. These loads can be PAYLOAD ELECTRICAL INTERFACES accurately determined via a coupled loads analysis. Starship will replicate common payload power and data For payload specific loads or rideshare loads interface standards on the flight vehicle in lieu of assessments, contact [email protected]. customer-provided electrical ground support equipment (EGSE) for final pre-launch operations. This will allow the payload to be powered, monitored, and © Space Exploration Technologies Corp. All rights reserved. 3

STARSHIP PAYLOAD GUIDE ACOUSTICS SHOCK During flight, the payload will be subjected to a range SpaceX is designing Starship to have benign shock of acoustic environments. Levels are highest during environments. Stage separation and payload fairing liftoff and transonic flight, due to acoustic and door opening will generate negligible shock aerodynamic excitations. The maximum expected environments at the payload interface. Consequently, payload acoustic environments are shown in Table 1 the maximum shock environment is typically due to the and Figure 6 in one-third octave bands. Contact payload separation system selected for the mission. [email protected] for mission specific low frequency Typical maximum shock levels at the payload acoustic assessments. separation plane induced by payload separation Frequency Acoustic Limit Levels systems are provided in Table 2 below. (Hz) 1/3 Octave Frequency Shock SRS 100 130 (Hz) (g-peak) 125 130 100 20 160 130 1000 1000 200 130 10000 1000 250 129 Table 2: Typical payload separation-induced shock at 315 127 the payload separation plane 400 124.5 500 122 630 118.5 PAYLOAD INTEGRATION 800 115.5 SpaceX is initially planning for two launch sites for the 1000 113 Starship vehicle: 1250 111 1600 109.5  Kennedy Space Center LC-39A | 28.6082° N 2000 108.5 latitude, 80.6041° W longitude 2500 107.5  Boca Chica launch pad | 25.9971° N latitude, 3150 106.5 97.1554° W longitude 4000 105.5 For payloads requiring return to Earth, landing sites are 5000 104.5 coordinated with SpaceX and could include Kennedy 6300 103.5 Space Center, FL or Boca Chica, TX. 8000 102.5 Payloads are integrated into the Starship fairing 10000 101.5 vertically in ISO Class 8 (Class 100,000) cleanrooms. OASPL (dB) 137.7 Then the integrated payload stack is transferred to the Table 1: Payload acoustic environment (1/3 octave) launch pad and lifted onto the Starship vehicle, while maintaining the same vertical orientation throughout the entire process. Conditioned air is delivered into the fairing during encapsulated ground processing while in the processing facility and on the launch pad. PAYLOAD SEPARATION SpaceX provides in-flight commanding and monitoring of the payload separation system(s). Starship can perform 3-axis attitude controlled or spin-stabilized spacecraft separation. Note that certain spacecraft separation maneuvers may reduce available payload volume. Collision avoidance maneuvers will be performed as required. Figure 6: Payload acoustic environment (1/3 octave) © Space Exploration Technologies Corp. All rights reserved. 4

STARSHIP PAYLOAD GUIDE PERFORMANCE CREW CONFIGURATION The Starship and Super Heavy system offers SpaceX was founded with the goal of making life multi- substantial mass-to-orbit capabilities. At the baseline planetary. The Starship program is realizing this goal reusable design, Starship can deliver over 100 metric with the crew configuration of Starship. Drawing on tons to LEO. Utilizing parking orbit refueling, Starship experience from the development of Dragon for the is able to deliver unprecedented payload mass to a Commercial Crew Program, the Starship crew variety of Earth, cislunar, and interplanetary configuration can transport up to 100 people from Earth trajectories. A summary of available Starship into LEO and on to the Moon and Mars. The crew capabilities is provided in Table 3 below. The single configuration of Starship includes private cabins, large launch mass-to-orbit assumes no orbital refueling of common areas, centralized storage, solar storm Starship. The maximum mass-to-orbit assumes shelters and a viewing gallery. parking orbit propellant transfer, allowing for a substantial increase in payload mass. These performance numbers assume full Starship reuse, including Super Heavy return to launch site. For performance estimates to a specific orbit, please contact [email protected]. Orbit Mass-to-Orbit Mass-to- Single Launch Orbit Prop Transfer (t) LEO1 100+ 100+ GTO2 21 100+ Lunar Surface N/A 100+ Figure 8: Starship Crew Configuration Mars Surface N/A 100+ 1 Up to 500-km circular orbit at up to 98.9-deg inclination 2Assumes 185 x 35,786 km orbit at 27-deg inclination with 1800 m/s V to go Table 3: Expected Starship Performance ADDITIONAL CAPABILITIES Fully-reusable Starship and Super Heavy systems are expected to allow for space-based activities that have CARGO CONFIGURATION not been possible since the retirement of the Space Starship was designed from the onset to be able to Shuttle and Space Transportation System or have carry more than 100 tons of cargo to Mars and the never been possible before. With a fully reusable Moon. The cargo version can also be used for rapid Starship, satellites can be captured and repaired in point-to-point Earth transport. Various payload bay orbit, returned to Earth, or transferred to a new configurations are available and allow for fully operational orbit. For more information on additional autonomous deployment of cargo to Earth, Lunar, or capabilities or to conceptualize new ideas, please Martian surfaces with one example shown in Figure 7. contact [email protected]. Figure 7: Cargo Starship on Lunar Surface © Space Exploration Technologies Corp. All rights reserved. 5