Thursday, December 18, 2014

PocketQubeShop announces PocketQube Kit v1.0 EM

PocketQubeShop announces PocketQube Kit v1.0 EM
PocketQubeShop, 18 December 2014
http://www.pocketqubeshop.com/hardware/pocketqube-kit

A kit containing the following components

  • Alba Orbital Skeletonized structure (1p, 2p or 3p)
  • Radiobro MiniSatCom
  • Alba Orbital Labsat (Test and Development Board)
  • Alba Orbital On Board Computer (OBC)

Wednesday, December 10, 2014

Graham Sortino's Rocket Work

Small-Liquid-Fueled-Rocket-Engines on Fubar Labs Site

http://wiki.fubarlabs.org/fubarwiki/Small-Liquid-Fueled-Rocket-Engines.ashx

Graham Sortino has been very busy with his small rocket projects. He's been making great progress. Here's a list of some of them. Check out his progress.

  • Igniters:
    • Air / Ethanol Igniter Engine (2012)
    • Gaseous Oxygen (GOX) / Ethanol Igniter Engine (2012)
    • GOX / Ethanol Igniter v2 (2014)
    • GOX / Ethanol Igniter v3 3D Printed (2014)
  • Engines:
    • 3D Printed Engine (2014)
  • Software & Hardware
  • Rocket Engine Test Stand
  • Propellant Flow Testing
  • Thermal Analysis of Steady State Engines (Cooling)

CS BPM-5 Rocket Motor Model

Copenhagen Suborbitals' BPM-5 Rocket Motor Model
sketchfab, 10 December 2014
https://sketchfab.com/models/78c96477043247c7bc807989391510df

An interactive model of the Copenhagen Suborbitals' BPM-5 Rocket Motor. It is similar to an LR-101. You can zoom in and pan over the model.

Friday, November 28, 2014

Video: Toroidal Tank Development Program

HACL Film 00031 Toroidal Tank Development Program, for Saturn Launch Vehicle
YouTube, 28 November 2014
https://www.youtube.com/watch?v=FqxEy_kszD0

This video shows the development of toroidal tanks through the full design and development cycle.

Wednesday, October 29, 2014

Dozens of CubeSats lost in Antares rocket failure

Dozens of CubeSats lost in Antares rocket failure
Electronics Weekly, 29 October 2014
http://www.electronicsweekly.com/news/military-aerospace-electronics/dozens-cubesats-lost-antares-rocket-failure-2014-10/

Alongside NASA’s Cygnus cargo pod, dozens of CubeSats were destroyed in the Antares rocket launch failure. Among them were 26 Dove earth-observation CubeSats from Planet Labs, known as Flock-1d

Thursday, October 16, 2014

NASA Nanolaunch 1200 Resources

Nano Launch 1200: MSFC's Role and Vision for Small Launch Vehicles

David Manual Dominguez's Orbital Launch Vehicle Workshop report

NanoLaunch 1200 to ADAS Enabling Affordable, Dedicated Access to Space Through Aggressive Technology Maturation

UAH Charger Rocket Works/ Prometheus Student Launch Team Report

Experimental and Computational Investigation of a Dual-Bell Nozzle

Pat Lampton: Nanolaunch Phase 1 flight Video

Life Cycle Analysis of Dedicated Nano-Launch Technologies

Life Cycle Analysis of Dedicated Nano-Launch Technologies
NASA, 16 October 2014
http://science.ksc.nasa.gov/shuttle/nexgen/Nexgen_Downloads/CRASTE_Zapata_et_al_Paper_Assess_Dedicated_Nano-Launch_r8.pdf

ABSTRACT

Recent technology advancements have enabled the development of small cheap satellites that can perform useful functions in the space environment. Currently, the only low cost option for getting these payloads into orbit is through ride share programs - small satellites awaiting the launch of a larger satellite, and then riding along on the same launcher. As a result, these small satellite customers await primary payload launches and a backlog exists. An alternative option would be dedicated nano-launch systems built and operated to provide more flexible launch services, higher availability, and affordable prices. The potential customer base that would drive requirements or support a business case includes commercial, academia, civil government and defense. Further, NASA technology investments could enable these alternative game changing options.

With this context, in 2013 the Game Changing Development (GCD) program funded a NASA team to investigate the feasibility of dedicated nano-satellite launch systems with a recurring cost of less than $2 million per launch for a 5 kg payload to low Earth orbit. The team products would include potential concepts, technologies and factors for enabling the ambitious cost goal, exploring the nature of the goal itself, and informing the GCD program technology investment decision making process.

This paper provides an overview of the life cycle analysis effort that was conducted in 2013 by an inter-center NASA team. This effort included the development of reference nano-launch system concepts, developing analysis processes and models, establishing a basis for cost estimates (development, manufacturing and launch) suitable to the scale of the systems, and especially, understanding the relationship of potential game changing technologies to life cycle costs, as well as other factors, such as flights per year.