surface-to-surface power beaming · ancillary services are frequency agnostic, with a ka band...
TRANSCRIPT
Does your Payload Need Power & Ancillary Services To Operate and
Survive the Night?
Are power, mass, volume, data, navigation, cadence, and/or related system complexity issues
impacting your science yield?
Does your ISRU application need sustainable energy generation, storage, and distribution
infrastructure?Contact [email protected] Innovative Space Partnerships, Inc.
www.xisp-inc.com
Surface-to-Surface Power Beaming
XISP-Inc Is seeking customers In need of power and ancillary services on the lunar
surface as well as lander partners that can accommodate our evolving power
and ancillary services beaming infrastructure
Power & Ancillary ServicesBeaming Technology Development,
Demonstration, and Deployment (TD3) Mission
Initial Payload SpecificationsMass: Less than 15 kg on landerVolume: 6U without deployment optionsInput Power Range: 10 to 1000 WReceived power is a function of input power, achievable power density, and distance. Ancillary services are frequency agnostic, with a Ka band nominal baseline.Adaptable Lander & Customer Interfaces
XISP-Inc Proposed LSITP Power & Ancillary Services Beaming Payload
ConformalTransceiver
1-Axis GimbalTransceiver
3-Axis GimbalTransceiver
pd is the power density at the center of the receiving location
𝑃𝑡 is the total radiated power from the transmitter
𝐴𝑡 is the total area of the transmitting antenna
λ2 is the wavelength squared
𝐷2 is the separation between the apertures squared
1 - Barnhard, Gary Pearce Space-to Space Power Beaming AIAA Space 20172 - William C. Brown, Life Fellow, IEEE, and E. Eugene Eves, Beamed Microwave Power Transmission and its Application to Space, IEEE Transactions On Microwave Theory and Techniques, Vol. 40, No. 6. June 1992
pd=𝐴𝑡𝑃𝑡
λ2𝐷2
Beaming Power Density and the Solar Constant
© 2019 XISP-Inc, All rights reserved
Reflectarray PV/Rectenna/Tx&Rx Apertures ISRU WaterWitch Lunar Regolith Processing Concept Scaled Sustainable Infrastructure