Skip to content
DefDex
NewRocket logo

Startup · Israel

NewRocket

HQ Netanya, IsraelFounded 201411-50 employeesUpdated

Technion spin-off founded in 2014 to develop rocket engines and gel propulsion technology for space and aviation markets.

Website

Funding2 rounds · $1.7M

Equity raised
$1.7M
Latest
$1.0MSeries A · Nov 30, 2020
Cumulative raised$1.7M
Feb 1, 2014Nov 30, 2020
  • Series A
    $1.0M
    Nov 30, 2020
  • Seed
    $700K
    Feb 1, 2014

Raised counts equity rounds; debt, secondary sales and grants are totaled separately. Amounts in other currencies are converted at the announcement month's average rate. A ~ marks an estimated or converted amount.

Capabilities2

  • Developer
    classify_sectors run 37, haiku, taxonomy 2026-10-18b: Develops rocket engines and gel propulsion for space and aviation markets; no defense use stated.
    —Reported
  • Developer
    classify_sectors run 37, haiku, taxonomy 2026-10-18b: Develops rocket engines and gel propulsion for space and aviation markets; no defense use stated.
    —Reported

Maturity and TRL describe this organization's work; the field-wide maturity is on each technology's page.

People
PersonRole
Moti ElyashivCo Founder & Director
Zohar SchlagmanCo-Founder & Chief Technology Officer
Ilan HarelChief Executive Officer

Sources4

Profile3

  1. 1

    Supports Organization · description

    “Founded in 2014, NewRocket is a Technion spin-off developing rocket engines for the space and aviation markets.”
  2. 2

    NewRocket · Supports Organization · website

    “NewRocket’s thrusters and propellants are primarily intended for in-space propulsion systems that require precision maneuverability with powerful performance”
  3. 3

    Supports Organization · name

    “Zohar Schlagman, NewRocket Ltd”

Funding1

  1. 4

    Octen Business Search · Supports Funding round, Organization · country, Organization · employee range, Organization · hq city, Organization · linkedin url, Role

    “funding round: Series A, 2020-11-30, USD 1,000,000”

Each fact on this page is attached to the sources that support it. Archived copies are linked when we keep one.