SBIR-STTR Award

Low Cost Nano and Micro Satellite Launch Stage and Automated Hypersonic Test Platform
Award last edited on: 3/16/23

Sponsored Program
SBIR
Awarding Agency
NASA : MSFC
Total Award Amount
$124,290
Award Phase
1
Solicitation Topic Code
Z9.01
Principal Investigator
Mark C Russell

Company Information

HyperSciences Inc

522 North Fiske Street Suite 1
Spokane, WA 99202
   (509) 994-8577
   info@hypersciences.com
   www.hypersciences.com
Location: Single
Congr. District: 05
County: Spokane

Phase I

Contract Number: 80NSSC18P2229
Start Date: 7/27/18    Completed: 2/15/19
Phase I year
2018
Phase I Amount
$124,290
HyperSciences, Inc. is proposing is a robust, cost effective, automated hypersonic launch system and encapsulated projectile bus capable of delivering small payloads to altitudes as high as 100Km. HyperSciences uses our proven, existing and patented Ram accelerator-based launch architecture and in-ground launch site based at Spaceport America to launch payloads at greater than Mach 5. This cost-effective launch vehicle enables cheap access to high altitude and space, providing on-demand launches. One novel feature of the Ram accelerator is a fully tailorable G-load profile with length and simple gas propellant selection. Because of the loads experienced during launch minor G-load toughening of existing payloads are only required, as a result a new class of tough, low-cost payloads will emerge to be able to be flown on this system. The reduction of cost and the ability to have on demand launch services will further strengthen and accelerate the developing small satellite and hypersonic test vehicle market. Some of the key innovations in this technology which allow the impulsive launch are: Automated hypersonic testing platform for stage 1 launch replacement and hypersonic testing Heat resistant aero shell to help protect payload and upper stages Extendable features to allow for stable flight throughout launch “Egg carton” technology to help share acceleration load throughout the structure Potential NASA Applications Payloads could be flight tested on board the launch vehicle prior to being integrated into larger launch system. Exposure of the payload to the moderate g-loads of the impulsive launch would provide for an effective test of payload robustness. The mass driver can be readied for launch in a matter of minutes which would provide game- changing responsiveness in satellite launch. The lifetime of satellites could be reduced because the cost & time to launch a replacement satellite would be very low Potential Non-NASA Applications By reducing the cost of building and launching satellites, satellite-based internet and communication everywhere on the planet would become more feasible. Many Nano or Micro satellites in orbit would also have many benefits in the arena of video monitoring, defense, agriculture, etc. The barrier to space access will be lowered both from an economic and a technological standpoi

Phase II

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Start Date: 00/00/00    Completed: 00/00/00
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