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Orbital Express Space Operations Architecture Program

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Orbital Express Space Operations Architecture Program SSC03-IV-2 Orbital Express Space Operations Architecture Program James Shoemaker Defense Advanced Research Projects Agency, 3701 N Fairfax Drive, Arlington, VA, USA 22203 [email protected], 703-696-2368 Melissa Wright, Sanjivan Sivapiragasam SRS Technologies, 4001 N Fairfax Drive, Arlington, VA, USA 22203 [email protected], 703-284-7782; [email protected], 703-284-7788 ABSTRACT . The goal of the Orbital Express Space Operations Architecture program is to validate the technical feasibility of robotic, autonomous on-orbit refueling and reconfiguration of satellites to support a broad range of future U.S. national security and commercial space programs. Refueling satellites will enable frequent maneuvers to improve coverage, change arrival times to counter denial and deception, and improve survivability, as well as extend satellite lifetime. Electronics upgrades on-orbit can provide performance improvements and dramatically reduce the time to deploy new technology. The Orbital Express advanced technology demonstration will design, develop, and test on orbit a prototype servicing satellite (ASTRO), a surrogate next generation serviceable satellite (NEXTSat). The elements of the Orbital Express demonstration will be tied together by non-proprietary satellite servicing interfaces (mechanical, electrical, etc.) that will facilitate the development of an industry wide on-orbit servicing infrastructure. NASA will apply the sensors and software developed for autonomous rendezvous and proximity operations to enable future commercial resupply of the International Space Station. Keywords: satellite servicing, autonomous rendezvous 1. Introduction The Orbital Express program is envisioned to set the mission performance more efficiently than through stage for the establishment of an on-orbit satellite block replacements of satellite constellations. servicing infrastructure for routine, cost-effective, autonomous capability for resupply and reconfiguration DARPA’s vision of post-2010 space operations of on-orbit spacecraft in the post-2010 timeframe. An foresees satellites designed and equipped with Orbital Orbital Express-derived satellite servicing architecture Express-derived standard mechanical and electrical will usher in a revolution in space operations, enabling interfaces enabling automated receipt of fluid new and enhanced satellite capabilities supporting not consumables (fuel and cryogens) and upgraded only national security missions, but civil and electronic components via an unmanned servicing commercial space activities as well. spacecraft (Autonomous Space Transfer and Robotic Orbiter vehicle, or ASTRO). ASTRO will also be Routine, autonomous satellite servicing will provide capable of refueling microsatellites. spacecraft with unprecedented freedom of maneuver, allowing satellite coverage to be adjusted or optimized In order to take advantage of an on-orbit servicing at will, or enabling spacecraft to employ unpredictable infrastructure, the next generation of satellites maneuvers to counter possible threats or adversary (NEXTSats) will have to be designed to enable routine, activity scheduling. Routine, autonomous, preplanned autonomous on-orbit servicing. A non-proprietary, upgrades or reconfiguration of spacecraft components “open” industry standard for satellite-to-satellite will dramatically reduce the "time to market" of new servicing interfaces must be adopted to ensure on-orbit technology into operational satellites, increasing servicing compatibility among ASTROs and NEXTSats Approved for Public Release, Distribution Unlimited – DARPA Case #43484 Page 1 James Shoemaker 17th Annual AIAA/USU Conference on Small Satellites designed and produced by different manufacturers. revolution in both system acquisition and in the NEXTSats must also be designed such that fluid flexibility with which national security, civil and transfer interfaces and Orbital Replacement Unit (ORU) commercial space systems are employed. The installation ports are unobstructed and readily demonstration will develop and validate technologies accessible by an autonomous servicing spacecraft. which are critical to the establishment of an operational satellite servicing system, convincingly showing that The Orbital Express Advanced Technology the Orbital Express vision is technically feasible, Demonstration (ATD) program will facilitate the sufficiently mature, and will provide the mission utility realization of this vision of routine, autonomous on- and operational value that future customers will require. orbit satellite servicing, and in so doing will prompt a 2. Operational System Vision Orbital Express will establish a revolutionary approach for national security, civil and commercial space to new space architectures, providing a cost-effective activities. method for autonomous satellite servicing, using a standard industry-wide interface. Future systems that make use of this servicing capability will have many advantages over traditional DARPA envisions an operational Orbital Express spacecraft architectures. Satellites will be able to satellite servicing system which will revolutionize maneuver on demand to improve coverage, avoid space operations by providing a routine, cost-effective, threats, or surprise adversaries with unpredictable fly- autonomous capability to resupply satellites in the post- over times. Earlier operational capability will be 2010 timeframe. The capability to refuel satellites will possible with a partially deployed constellation. Fully enable more frequent maneuvering, allowing coverage functional satellites will be able to be rescued from to be adjusted as needed. The capability to replace delivery to the wrong orbital location. Failed or electronics will reduce the “time to market” for new degraded satellites will be repaired or refueled to technology by allowing spacecraft to be upgraded as the restore full or partial capability. Satellites will be new parts become available, not waiting for the next repositioned or reconfigured to address changing block upgrade. This will increase spacecraft mission market needs. Larger and more sophisticated satellites performance, and will enable new satellite capabilities will be launched with minimum propellant onboard. Spacecraft Bus RPO Sensors Cargo Section Capture System Remote Manipulator Arm Module and Support Assembly Figure 1: Operational System ASTRO Approved for Public Release, Distribution Unlimited – DARPA Case #43484 Page 2 th James Shoemaker 17 Annual AIAA/USU Conference on Small Satellites As shown in Figure 1, the operational ASTRO servicer docking face to NEXTSat’s, and matching consists of a spacecraft bus with several servicing rotational rates. An optional crosslink allows elements: rendezvous and prox ops (RPO) sensors to ASTRO to notify NEXTSat of its approach, and to determine the location and attitude of the target confirm that NEXTSat is ready for servicing. At satellite; a capture system module which contains the this point, ASTRO can either “direct capture” by docking mechanism as well as fluid couplers and flying close to the client spacecraft and engaging electrical connectors; a robotic arm to transfer ORUs the capture mechanism, or it can stand off a and/or to grapple the target spacecraft from a larger distance from the client and engage the robotic arm stand-off distance; a cargo section to house the fluid to “grapple” the client spacecraft, then drawing it and ORUs being transferred from the commodities close to engage the capture mechanism. spacecraft (CSC) to the client spacecraft. 6. Mated Operations: Once mated, ASTRO initiates delivery of the The concept of operations (CONOPS) for a servicing required fluid and/or ORUs, coordinating activities architecture is based on a standard set of mission with NEXTSat via a hardline electrical connection. procedures and servicing elements for all missions, but Typically, the NEXTSat attitude control will be each mission/client will have an optimum combination disabled and ASTRO will provide attitude control of steps and elements. Notionally, a given ASTRO for the mated stack. would reside on orbit for years, ferrying supplies back 7. Release & Separation: and forth between disposable commodities depots and After servicing is completed, ASTRO releases multiple client spacecraft in a constellation, but the NEXTSat from the capture mechanism and backs architecture can easily be modified to accommodate a away, maintaining sensor lock to preclude wide range of servicing scenarios. The CONOPS is recontact between the two spacecraft. depicted in Figure 2, with a representative client 8. Loiter Orbit: spacecraft (NEXTSat) and commodities depot (CSC), While not actively engaged in servicing operations, and consists of the following elements: ASTRO resides in a loiter orbit somewhere below the NEXTSat. 1. Pre-launch / Mission Planning: 9. Deploy / Retrieve Microsat: Determine the CONOPS for that particular As required, ASTRO can deploy, refuel, or retrieve mission/client, including the type of servicing microsats. These microsats can be launched desired, the frequency of servicing required, the berthed in ASTRO, attached to a CSC, or by some optimum number and placement of servicers, etc other method. 2. Launch: 10. Rendezvous & Capture CSC: ASTRO is launched into an orbit near the ASTRO performs the same steps used to NEXTSat, fully loaded with fluid and/or ORUs. rendezvous with NEXTSat to rendezvous with the As needed, commodities depots are launched into a CSC. lower, but compatible, orbit. 11.
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