LOTUS

Standardized ESPA propulsion system

Chrishma Derewa, Scott Fisher, Amar Vora, Srikanth Raviprasad, Curtis Iwata, Mark A. Seymour

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The LOTUS (Lander/Orbiter Trans-Upper Stage) system proposes a low-cost transport vehicle to small bodies such as the Moon, asteroids, and comets using the Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA) ring. The ESPA ring was originally developed as a mounting structure to attach and deploy secondary payloads in low Earth orbit whilst having minimal impact on the primary mission. It has been used and flight qualified on Atlas V and Delta IV rockets, with numerous launches since its first flight on STP-1 in 2007. Similar to the original ESPA ring, LOTUS is designed to utilize excess mass capacity in future EELV launches. However, LOTUS will feature all of the systems required to make itself into a free-flying spacecraft, including propulsion, power, attitude control, processing, orbit determination, and communications systems. It will provide a standardized, low cost, flexible system capable of addressing various mission needs and requirements. As a transportation system, LOTUS will be capable of delivering multiple small payloads to their desired orbits around the moon and other nearby targets (for example, near-Earth asteroids). It will also feature capabilities to soft-land small vehicles on the surface of the moon. This paper will emphasize the integrated propulsion systems architecture for the LOTUS, as well as outline a nominal baseline mission to deliver a satellite into lunar orbit and rover to the surface of the Moon.

Original languageEnglish
Title of host publication51st AIAA/SAE/ASEE Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Print)9781624103216
Publication statusPublished - 01-01-2015
Externally publishedYes
Event51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015 - Orlando, United States
Duration: 27-07-201529-07-2015

Conference

Conference51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015
CountryUnited States
CityOrlando
Period27-07-1529-07-15

Fingerprint

Moon
Propulsion
Orbits
Asteroids
Launch vehicles
Spacecraft propulsion
Earth (planet)
Attitude control
Rockets
Mountings
Costs
Communication systems
Satellites
Processing

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Derewa, C., Fisher, S., Vora, A., Raviprasad, S., Iwata, C., & Seymour, M. A. (2015). LOTUS: Standardized ESPA propulsion system. In 51st AIAA/SAE/ASEE Joint Propulsion Conference American Institute of Aeronautics and Astronautics Inc. (AIAA).
Derewa, Chrishma ; Fisher, Scott ; Vora, Amar ; Raviprasad, Srikanth ; Iwata, Curtis ; Seymour, Mark A. / LOTUS : Standardized ESPA propulsion system. 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2015.
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Derewa, C, Fisher, S, Vora, A, Raviprasad, S, Iwata, C & Seymour, MA 2015, LOTUS: Standardized ESPA propulsion system. in 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015, Orlando, United States, 27-07-15.

LOTUS : Standardized ESPA propulsion system. / Derewa, Chrishma; Fisher, Scott; Vora, Amar; Raviprasad, Srikanth; Iwata, Curtis; Seymour, Mark A.

51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2015.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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M3 - Conference contribution

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Derewa C, Fisher S, Vora A, Raviprasad S, Iwata C, Seymour MA. LOTUS: Standardized ESPA propulsion system. In 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA). 2015