Lead Time:
6 months
Peak Payload Power (unregulated):
160 W
Type:
Flight Hardware
Peak Regulated Power:
500 W
Data Storage:
32 GB
Downlink:
<100 Mbps
Bus Voltage (independent of power subsystem):
3.3 to 30 V
Lifetime in GEO:
2 years
Energy Storage:
100 Wh
Uplink:
20 kbps
Lifetime in LEO:
5 years

Pumpkin’s flight proven SUPERNOVA architecture delivers first in class payload power and volume for a range of small satellite missions. SUPERNOVA is available in 3U, 6U, and 12U form factors with standard and custom solar array options and support for multiple RF (VHF, UHF, S-band, X-band) solutions. Precision pointing accuracy and arc-second pointing knowledge are achievable with standard ADCS options.

Form Factor 6U
Payload Volume 4U
Peak Solar Power (BoL) 68W

6U SUPERNOVA BUS

Pumpkin Space Systems

Pumpkin’s flight proven SUPERNOVA architecture delivers first in class payload power and volume for a range of small satellite missions. SUPERNOVA is available in 3U, 6U, and 12U form factors with standard and custom solar array options and support for multiple RF (VHF, UHF, S-band, X-band) solutions. Precision pointing accuracy and arc-second pointing knowledge are achievable with standard ADCS options.

Form Factor 6U
Payload Volume 4U
Peak Solar Power (BoL) 68W
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Lead Time:
6 months
Peak Payload Power (unregulated):
160 W
Type:
Flight Hardware
Peak Regulated Power:
500 W
Data Storage:
32 GB
Downlink:
<100 Mbps
Bus Voltage (independent of power subsystem):
3.3 to 30 V
Lifetime in GEO:
2 years
Energy Storage:
100 Wh
Uplink:
20 kbps
Lifetime in LEO:
5 years

Pumpkin’s flight proven SUPERNOVA architecture delivers first in class payload power and volume for a range of small satellite missions. SUPERNOVA is available in 3U, 6U, and 12U form factors with standard and custom solar array options and support for multiple RF (VHF, UHF, S-band, X-band) solutions. Precision pointing accuracy and arc-second pointing knowledge are achievable with standard ADCS options.

Form Factor 6U
Payload Volume 4U
Peak Solar Power (BoL) 68W