A recent SpaceNews article explains how LACMA's ENOCH CubeSat was tracked by CSpOC . ENOCH was somewhat unusual in that it was conceived as a purely passive CubeSat. In order to satisfy its launch license requirements, ENOCH integrated a small, battery-powered beacon, in the form of SRI International's CubeSat Identification Tag (CUBIT). A CUBIT was attached to ENOCH's structure late in the integration phase. For more info on ENOCH, see our news page or visit LACMA. For those in the know, ENOCH measured less than a cubit in length ...

Please visit us and learn about our new products designed and made in California in booth #6 at the SmallSat 2019 conference in Logan, Utah on Monday, August 5 through Thursday, August 8, 2019.

The BRRM mission for which Pumpkin provided the structure, OBC (MBM 1 + PPM E1), fixed and deployable solar panels, solar panel release mechanism (PRM, driven by the SIM module), and overall system integration, has an excellent mission overview page. Of particular note are some of these highlights:

• The manner in which the payload interfaced to the bus -- the payload (see Figure 4) interfaced to the bus solely by plugging into the bus via the CubeSat Kit (CSK) 104-pin connector, and was secured in place via mounting holes in the custom Pumpkin chassis.
• The overview of anomalous events and their resolutions (see Figure 9).
• The issue of the effect of resets on the Real-Time Clock (RTC). Since 2009, the RTC has lived on the Pumpkin Motherboard Module (MBM 1), and is provided with an independent RTC backup battery (VBACKUP), that can be source from either a BR1225 Lithium coin cell on the MBM 2, or by an external power source connected to VBACKUP on the CSK 104-pin bus. In both cases, the backup power to the RTC is through a series 10kOhm resistor, thereby limiting max power to 1mW. Unfortunately BRRM used neither of these options, and so the RTC would lose its state whenever there was a global power-system reset. Recent revisions to the CubeSat specification have incorporated an allowance for low-current 3V power  sources for RTCs; however, not all launch providers will allow this. We recommend that all RTC users push their launch providers hard to allow these low-energy, low-power, low-risk RTC backup sources.

NASA's ALBus CubeSat was launched from New Zealand on 16 December 2018. ALBus is a 3U CubeSat serving as a testbed for a high power electrical system, and the use of shape memory alloys (SMAs) in its solar panel hinges and release mechanism.

Pumpkin designed and built the ALBus solar panels to NASA GRC's specifications within a very short time period. Additionally, ALBus utilizes a Pumpkin CubeSat Kit 3U structure. While the fixed 7S1P panels were relatively standard in their layout, the deployable 7S1P panels had special design features to accommodate ALBus' SMA hinges and the SMA-based release mechanism. Pumpkin worked with NASA GRC early career engineers to resolve all of these special requirements in an elegant fashion. 

NASA has provided detailed technical information on ALBus and its development.

On 5 May 2019 a Rocket Lab Electron rocket launched three small satellites from New Zealand’s North Island. Included in the manifest is AFRL's SPARC-1, a 6U CubeSat built on Pumpkin's SUPERNOVA bus, with two payloads. This is the second SUPERNOVA launch, after 2015's SUPERNOVA-Beta launch that ended with the failure of the Super Strypi launch vehicle on Nov 3, 2015.

While SUPERNOVA-Beta remains in a sub-aqueous orbit, SPARC-1 is now in a LEO Orbit and undergoing commissioning.

JPL has now demonstrated a laser communications pointing experiment between two JPL small satellites: ISARA (the receiver) and OCSD (the transmitter). ISARA is a 3U CubeSat that is powered by a novel, deployable Pumpkin solar array that stows around three sides of the 3U structure. The array's three monolithic panels are hinged together, and deploy to present 24 solar cells on top, and a Ka-band reflectarray (that is essentially an RF Fresnel lens), on the bottom. The flatness of these three panels is critical for the performance ISARA's Ka-band system. 

ISARA was launched in January 2018. ISARA's solar array and reflectarray have functioned flawlessly on orbit. More information about the recent laser experiment is available here.

In 2018, Pumpkin was the exclusive provider of solar panels for NovaWurks' PODSAT, a short-duration GTO-class mission to validate several concepts of NovaWurks' cellular architecture. PODSAT's primary solar panels used are the exact same models as are currently flying in LEO on NovaWurks' eXCITe mission. Read more about PODSAT here.

On Monday, SpaceX delivered NovaWurks' eXCITe small satellite into LEO orbit. NovaWurks relayed to us on Tuesday that eXCITE's Pumpkin Deployable Clamshell Solar Arrays (DCSAs) using our PMDSAS technology had deployed, were delivering their expected power, and eXCITe was already operational. Small space has become truly responsive.

Pumpkin's relationship with NovaWurks harkens back to the NGC/NovaWorks Mayflower 3U CubeSat mission, for which Pumpkin built a deployable 56W solar array in 2009. No comparable array existed at that time; ten weeks after an initial meeting, Pumpkin had delivered the all-new functional array to NovaWorks, and in 2010 the LEO mission executed successfully, carrying the NGC/NovaWorks core 2U and an additional 1U payload named Caerus from USC/ISI. To date, Mayflower is apparently the highest power-to-weight spacecraft ever built (56W in 4kg), and Pumpkin's 56W array was a critical enabling component.

The 56W Mayflower array was the genesis for Pumpkin's current wide range of PMDSAS(TM) solar arrays. The Pumpkin DCSA on eXCITe uses the fifth generation of Pumpkin's PMDSAS solar panel technology, stows safely in its own clamshell, and when released, deploys to two independent strings of solar cells. ​

For this eXCITe mission, Pumpkin originally delivered two 112W DCSAs. By the time the various payloads of the eXCITe mission were finalized in 2018, Pumpkin had increased the power of each DCSA array to 176W within the same footprint, thereby demonstrating the overall versatility of the DCSA. Pumpkin also built the fixed solar panels on each HiSat cell in eXCITe. The DCSA and other space-proven Pumpkin PMDSAS solutions are available as COTS offerings.

We wish NovaWurks all the best in this holiday season, for their eXCITe mission. 

FLEET Space's Centauri 1 was deposited into its intended orbit by India's PSLV-C43 yesterday, and has already broadcast some initial health and status information.

​The Centauri CubeSats Pumpkin built for FLEET Space have best-in-class solar arrays, batteries and structural integrity, along with a 1GHz Linux C&DH platform. Centauri 1 & 2 are comprised of:
​

• Pumpkin CubeSat Kit Pro chassis structure
• Pumpkin PMDSAS deployable and fixed solar panels
• Pumpkin PRM panel release mechanisms
• Pumpkin SUPERNOVA bus stack (PIM, MBM 2 + BBB, GPSRM 1, RHM, SIM)
• Pumpkin BM 2 Intelligent Battery Module (86Wh)
• Third-party EPS, ADACS, simplex Globalstar beacon, UHF transceiver, UHF antenna
• FLEET Space radio payloads & antennas
• System software from FLEET Space, Pumpkin, Bright Ascension and Kubos.

You can see a video of the deployment of Centauri 1 from the PSLV upper stage here. Note the comparative lack of tipoff, especially compared to some other 3U CubeSats ... Here's another mention of the satellite and launch.

When FLEET Space had a last-minute opportunity to launch 3U  worth of CubeSats on a Rocket Lab Electron launch vehicle, with the caveat that the CubeSats had to be ready in two weeks (!), they came to Pumpkin. We not only typically have nanosatellite-class equipment in stock, but we also have a proven track record of working quickly on projects that require outside-of-the-box thinking.

Within two weeks, we needed to come up with a working architecture, source the required components / assemblies, make any modifications required, integrate the FLEET payload and antennas (the pixelated portion above), and provide a software framework upon which FLEET could write their mission software.

Given the very short notice and the desire to maximize the utility of the 3U of volume available on this ride, Pumpkin and FLEET settled on a dual-1.5U mission, with two hardware-identical 1.5U CubeSats. We decided to go with a battery-power-only architecture, as that reduced costs and complexity, and fits within the 1.5U available. Pumpkin immediately embarked on creating a new operating mode for our BM 2 battery; within a few days we had this up and running, and Proxima I/II were thus enabled. The two satellite were built with US and Australian teams working together and remotely, then environmentally tested with no issues, and finally delivered to Rocket Lab for LV integration.

Proxima's Pumpkin components included:

• Solid-wall 1.5U Chassis Walls, with various Proxima-specific modifications
• Solid-wall Base Plate Assembly and Cover Plate Assembly, again with Proxima-specific modifications
• PPM E3 (an update to PPM E1, with more code space) running Salvo RTOS 4
• Motherboard Module (MBM), to host PPM E3 and serve as the mission C&DH processor
• GPSRM 1 GNSS receiver, with built-in Vinti7 orbit propagator (OP)
• BM 2 battery module, with new firmware including sleep mode

 
The Pumpkin bus components occupy around half the volume and mass of each Proxima CubeSat; FLEET's payload(s) occupy the rest. The GPSRM along with its power-efficient ​orbit propagator enable Proxima's mission ops, and the low-power 16-bit PPM E3 PIC24 MCU running Salvo along with the BM 2 and its sleep mode guarantee an efficient use of the battery's available energy. Additionally, some of the code from Stanford University's QB50 project was donated to the Proxima mission, and lives on in Proxima I/II. More information on these CubeSats can be found here.