Digital Solid State Propulsion, LLC
Reno, NV, US· latest recorded location
Digital Solid State Propulsion, LLC is named on 13 US grants and 12 published applications in this corpus. Its most frequent classification is C06B (Explosives or thermic compositions).
- Granted patents
- 13
- Published applications
- 12
- Inventors
- 7
- Granted in 2026 so far
- 0
- Most recent grant
- 13 Mar 2018
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2011 | 0 | 2 |
| 2012 | 2 | 2 |
| 2013 | 3 | 1 |
| 2014 | 2 | 1 |
| 2015 | 1 | 4 |
| 2016 | 2 | 1 |
| 2017 | 2 | 0 |
| 2018 | 1 | 1 |
By publication year.
Technology areas
Share of 25 documents
- C06BExplosives or thermic compositions20
- F02KJet-propulsion plants7
- F42DBlasting6
- E21BEarth or rock drilling4
- F23RGenerating combustion products of high pressure or high velocity3
- F41AFunctional features or details common to both smallarms and ordnance3
- F42CAmmunition fuzes3
- Y10TTechnical subjects covered by former us classification2
- C06CDetonating or priming devices1
Recent patents
- Solid electrically controlled propellants13 Mar 2018US 9,914,671 B1
- Solid electrically controlled propellants21 Mar 2017US 9,598,324 B1
- Liquid electrically initiated and controlled gas generator composition3 Jan 2017US 9,534,880 B2
- Solid electrically controlled propellants5 Jul 2016US 9,382,168 B2
- Liquid electrically initiated and controlled gas generator composition3 May 2016US 9,328,034 B2
- Use of liquid and gel monopropellants for well stimulation19 Jul 2018US 2018/0202277 A1
- Liquid electrically initiated and controlled gas generator composition25 Aug 2016US 2016/0245633 A1
- Liquid electrically initiated and controlled gas generator composition24 Sep 2015US 2015/0266791 A1
- Electrically ignited and throttled pyroelectric propellant rocket engine5 Mar 2015US 2015/0059314 A1
- Electrode ignition and control of electrically ignitable materials19 Feb 2015US 2015/0047526 A1
Most cited
By later US patents
- Method and system for controlling solid propellant thrust20US 8,584,443 B12013
- Family of modifiable high performance electrically controlled propellants and explosives15US 8,888,935 B22014
- Controllable digital solid state cluster thrusters for rocket propulsion and gas generation13US 8,464,640 B22013
- Liquid electrically initiated and controlled gas generator composition12US 9,182,207 B22015
- High performance electrically controlled solution solid propellant11US 8,317,952 B22012