Cal_X-1_figures-1.pdf

Payload Item Volume, cm (L x W x H)

Mass, kg

Orb. avg.

power, W

(peak power)

Survival power, W

Cal-T

X-ray telescope, options 1/2 160 x 36 x 18 / 200 x 20 x 20

12 / 10 15 (20) 1

Electronics 10 x 10 x 10 2 5 (5) n/a Reserve 4 / 3 5 (5) 1 Accommodation Summary 18 / 15 25 (30) 2

Cal-S

1.5 keV Source 10 x 10 x 18 2 8 (10) n/a 6 keV Source 10 x 10 x 18 2 8 (10) n/a Electronics 10 x 20 x 10 2 5 (10) 1

Reserve 2 7 (7) 1 Accommodation Summary 8 30 (40) 2

Table 1: Cal X-1 Payload Allocation Requirments

[1] Orbital Average Power and Peak Power allocations are given at a reference voltage of 12VDC.

Cal X-1 RFI supporting figures and tables

Fig. 4: Cal-T Option 1 and Cal-S Left, mounted on a 4-port ESPA Grande Rideshare configuration utilizing the “pie” volume allocation, and Right, mounted vertically to require additional vertical ESPA ring volume.

Fig. 5: Cal-T option 2. Four 12U cubesat dispensers shown mounted on a plate on a single ESPA Grande port. Cal-T and Cal-S occupy two of the dispensers and are deployed in rapid succession.

Fig. 6: Three Phases of Science Operations

Fig. 7: Mission Operations Diagram